Washington, U.S. National Aeronautics and Space Administration, Springfield, Va., for sale by the National Technical Information Service, 1976
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Washington, U.S. National Aeronautics and Space Administration, Springfield, Va., for sale by the National Technical Information Service, 1976
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The event Washington, U.S. National Aeronautics and Space Administration, Springfield, Va., for sale by the National Technical Information Service, 1976 represents a publication, printing, distribution, issue, release or production of resources found in Indiana State Library.
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Context of Washington, U.S. National Aeronautics and Space Administration, Springfield, Va., for sale by the National Technical Information Service, 1976Publication of
- 20- and 30-GHz millimeter wave experiments with the ATS-6 satellite, Louis J. Ippolito ; Goddard Space Flight Center, Greenbelt, Md
- A Hybrid computer program for rapidly solving flowing or static chemical kinetic problems involving many chemical species, Allen G. McLain and C. S. R. Rao ; Langley Research Center, Hampton, Va
- A balloon ozone measurement utilizing an optical absorption cell and an ejector air sampler, Ernest Hilsenrath and Thomas E. Ashenfelter ; Goddard Space Flight Center, Greenbelt, Md
- A comparison of matrix methods for calculating eigenvalues in acoustically lined ducts, Willie Watson and Donald L. Lansing ; Langley Research Center, Hampton, Va
- A computational system for aerodynamic design and analysis of supersonic aircraft : part 1-general description and theoretical development, W. D. Middleton, and J. L. Lundry ; prepared by Boeing Commercial Airplane Company, Seattle, Wash. for Langley Research Center
- A computational system for aerodynamic design and analysis of supersonic aircraft : part 3-computer program description, W. D. Middleton, J. L. Lundry and R. G. Coleman ; prepared by Boeing Commercial Airplane Company, Seattle, Wash. for Langley Research Center
- A computer program for anisotropic shallow-shell finite elements using symbolic integration, C. M. Andersen and John T. Bowen ; Langley Research Center, Hampton, Va
- A computer program to predict rotor rotational noise of a stationary rotor from blade loading coefficients, Ramani Ramakrishnan, Donald Randall, and Robert N. Hosier ; Langley Research Center, Hampton, Va
- A fuselage/tank structure study for actively cooled hypersonic cruise vehicles--summary, C. J. Pirrello, A. H. Baker, and J. E. Stone ; prepared by McDonnell Douglas Corporation for Langley Research Center
- A handbook for the estimation of airside delays at major airports (quick approximation method), Amedeo R. Odoni and Peeter Kivestu ; prepared by Massachusetts Institute of Technology, Cambridge, Mass., for Langley Research Center
- A numerically efficient finite element hydroelastic analysis : volume 1--theory and results, Robert N. Coppolino ; prepared by Grumman Aerospace Corporation, Bethpage, N.Y., for Langley Research Center
- A single field of view method for retrieving tropospheric temperature profiles from cloud-contaminated radiance data, Donald B. Hodges ; prepared by Texas A and M University, College Station, Tex., for George C. Marshall Space Flight Center
- A spacecraft-borne gradiometer mission analysis, P. Argentiero and R. Garza-Robles ; Goddard Space Flight Center, Greenbelt, Md
- A study of meteor spectroscopy and physics from earth-orbit : preliminary survey into ultraviolet meteor spectra, David D. Meisel
- A study of turbulent flow between parallel plates by a statistical method, R. Srinivasan ... [and others] ; prepared by Georgia Institute of Technology, Atlanta, Ga., for Langley Research Center
- A summary of the skylab crew : vehicle disturbances experiment T-013, Bruce A. Conway and T. C. Hendricks, Langley Research Center
- ADP correspondence system, unsolicited proposal evaluation tracking application : users manual and documentation, W. A. Greene, and D. J. Goodwin ; NASA Headquarters, Washington, D.C
- Acoustic, performance, and wake survey measurements of a lobed velocity-decayer nozzle installed on a quieted TF-34 turbofan engine, Nick E. Samanich and Laurence J. Heidelberg ; Lewis Research Center, Cleveland, Ohio
- Adaptation to prolonged bedrest in man : a compendium of research, John E. Greenleaf ... [and others]
- Advanced control technology and its potential for future transport aircraft, Dryden Flight Center, Edwards, Calif
- Aerodynamic characteristics of a 1/6-scale of the rotor systems research aircraft with the rotors removed, Raymond E. Mineck, Carl E. Freeman, and James L. Hassell, Jr. ; Langley Research Center, Hampton, Va
- Aerodynamic performance of 0.4066-scale model of JT8D refan stage, Royce D. Moore, George Kovich, and Edward R. Tysl ; Lewis Research Center, Cleveland, Ohio
- Aerodynamic performance of flared fan nozzles used as inlets, Donald A. Dietrich, Theo G. Keith, and Gary G. Kelm ; Lewis Research Center, Cleveland, Ohio
- Aircraft motion and passenger comfort data from scheduled commercial airline flights, Marta G. Gruesbeck and Daniel F. Sullivan
- An analytical study of turbulence responses, including horizontal-tail loads, of a control-configured vehicle with relaxed static stability, Boyd Perry ; Langley Research Center, Hampton, Va
- An equivalent energy for the outgassing of space materials, John J. Scialdone ; Goddard Space Flight Center, Greenbelt, Md
- An exact transformation from geocentric to geodetic coordinates for nonzero altitudes, David R. Hedgley, Jr. ; Flight Research Center, Edwards, Calif
- An experimental investigation of end treatments for nonreturn wind tunnels, William T. Eckert, Kenneth W. Mort, and J. E. Piazza ; Ames Research Center and U.S. Army Air Mobility R & D Laboratory, Moffett Field, Calif
- An inexpensive economical solar heating system for homes, Johnny W. Allred ... [and others] ; Langley Research Center, Hampton, Va
- An investigation of correlation between pilot scanning behavior and workload using stepwise regression analysis, Marvin C. Waller ; Langley Research Center, Hampton, Va
- An investigation of several NACA 1-series inlets at Mach numbers from 0.4 to 1.29 for mass-flow ratios near 1.0, Richard J. Re. ; Langley Research Center, Hampton, Va
- An investigation of size-dependent concentration of trace elements in aerosols emitted from the oil-fired heating plants, Jag J. Singh, R. J. Sentell, and G. S. Khandelwal ; Langley Research Center, Hampton, Va
- Analysis and design of a cantilever-mounted resilient-pad gas-lubricated thrust bearing, Izhak Etsion ; Lewis Research Center, Cleveland, Ohio
- Analysis of experimental results of the inlet for the NASA hypersonic research engine aerothermodynamic integration model, Earl H. Andrews, and Ernest A. Mackley ; Langley Research Center, Hampton, Va
- Apollo experience report - lunar-sample processing in the lunar receiving laboratory, high-vacuum complex, David R. White ; Lyndon B. Johnson Space Center, Houston, Texas
- Apollo experience report : guidance and control systems, Raymond E. Wilson, Jr. ; Lyndon B. Johnson Space Center, Houston, Texas
- Apollo experience report--crew station integration : volume I-- crew station design and development, Louis D. Allen and Dale A. Nussman ; Lyndon B. Johnson Space Center, Houston, Tex
- Apollo experience report--environmental acceptance testing, Charles H. M. Laubach; Lyndon B. Johnson Space Center, Houston, Texas
- Application of remotely sensed multispectral data to automated analysis of marshland vegetation, William G. Cibula ; Lyndon Space Center, Houston, Tex
- Approximate method for calculating transonic flow about lifting wing-body configurations, Richard W. Barnwell ; Langley Research Center, Hampton, Va
- Approximation concepts for efficient structural synthesis, Lucien A. Schmit and Hirokazu Miura ; prepared by University of California, Los Angeles for Langley Research Center
- Atmospheric structure and variability in areas of convective storms determined from 3-h rawinsonde data, Gregory S. Wilson and James R. Scoggins
- Axial jet mixing of ethanol in spherical containers during weightlessness, John C. Aydelott ; Lewis Research Center, Cleveland, Ohio
- Boundary-layer bleed system study for a full-scale, mixed-compression inlet with 45 percent internal contraction, Robert J. Shaw, Joseph F. Wasserbauer, and Harry L. Neumann ; Lewis Research Center, Cleveland, Ohio
- Calculation of subsonic and supersonic steady and unsteady aerodynamic forces using velocity potential aerodynamic elements, John Kenneth Haviland and Young Sik Yoo ; prepared by University of Virginia, Charlottesville, Va., for Langley Research Center
- Carbide coated fibers in graphite-aluminum composites, Richard J. Imprescia ... [and others] ; prepared by Los Alamos Scientific Laboratory, Los Alamos, N.M., for Langley Research Center
- Characteristics of the NASA Lewis bumpy-torus plasma generated with positive applied potentials, J. Reece Roth, Glenn A. Gerdin, and Richard W. Richardson ; Lewis Research Center, Cleveland, Ohio
- Characteristics of wake vortex generated by a Boeing 727 jet transport during two-segment and normal ILS approach flight paths, R. L. Kurkowski, M. R. Barber, and L. J. Garodz ; Ames Research Center, Moffett Field, Calif
- Classification software technique assessment, Robert R. Jayroe, Jr. ... [and others] ; George C. Marshall Space Flight Center
- Collected works of Robert T. Jones, Ames Research Center, Moffett Field, Calif
- Combustion of hydrogen injected into a supersonic airstream : a guide to the Hiss computer program, D. F. Dyer, G. Maples, and D. B. Spalding
- Comparison of types A and C fluorinated ethylene propylene (FEP) as cover materials for silicon solar cells, Jacob D. Broder ; Lewis Research Center, Cleveland, Ohio
- Computation of scalar far-field patterns of large-aperture antennas, Thomas A. O'Malley ; Lewis Research Center, Cleveland, Ohio
- Computer subroutines for the estimation of nuclear reaction effects in proton-tissue-dose calculations, John W. Wilson, and G. S. Khandelwal ; Langley Research Center, Hampton, Va
- Conceptual design study of 1985 commercial tilt rotor transports : volume III--Stol design summary, K. W. Sambell ; prepared by Bell Helicopter Company, Fort Worth, Tex., for Ames Research Center
- Cooled-turbine aerodynamic performance prediction from reduced primary to coolant total-temperature-ratio results, Louis J. Goldman ; Lewis Research Center, Cleveland, Ohio
- Correlations for determining thermodynamic properties of hydrogen-helium gas mixtures at temperatures from 7000 to 35 000 K, Ernest V. Zoby, Peter A. Gnoffo, and Randolph A. Graves, Jr. ; Langley Research Center, Hampton, Va
- Data for NASA's AVE IV experiment : 25 mb sounding data and synoptic charts, Nancy F. Fucik and Robert E. Turner ; George C. Marshall Space Flight Center, Marshall Space Flight Center, Ala
- Data for NASA's AVSSE II experiment : 25 mb sounding data and synoptic charts, Nancy F. Fucik and Robert E. Turner ; George C. Marshall Space Flight Center, Marshall Space Flight Center, Ala
- Defining constants, equations, and abbreviated tables of the 1975 U.S. standard atmosphere, R. A. Minzner ... [and others] ; Goddard Space Flight Center, Greenbelt, Md
- Design of a 4-1/2 stage turbine with a stage loading factor of 4.66 and high specific work output, P. F. Webster
- Development of a computer code for calculating the steady super/hypersonic inviscid flow around real configurations : volume I-computational technique, Frank Marconi, Manuel Salas, and Larry Yaeger ; prepared by Grumman Aerospace Corporations, Bethpage, N.Y
- Development of a computer code for calculating the steady super/hypersonic inviscid flow around real configurations : volume II - code description, Frank Marconi, and Larry Yaeger ; prepared by Grumman Aerospace Corporation, Bethpage, N.Y. for Langley Research Center, Hampton, Va
- Development of an optimal automatic control law and filter algorithm for steep glideslope capture and glideslope tracking, Nesim Halyo ; prepared by University of Virginia, Charlottesville, Va., for Langley Research Center
- Dynamics and identification on flexible aircraft, William R. Wells ; prepared by University of Cincinnati, Cincinnati, Ohio, for Langley Research Center
- Effect of Kruger nose flaps on the experimental force and moment characteristics of an oblique wing, Edward J. Hopkins and George H. Lovette ; Ames Research Center, Moffett Field, Calif
- Effect of Reynolds number on the aerodynamic stability and control characteristics of a 55 degree clipped-delta-wing orbiter configuration at supersonic Mach numbers, A. B. Blair, Jr. ; Langley Research Center, Hampton, Va
- Effect of Reynolds number on the subsonic boattail drag of several wing-body configurations, David E. Reubush ; Langley Research Center, Hampton, Va
- Effect of casing treatment on performance of an inlet stage for a transonic multistage compressor, Donald C. Urasek, George W. Lewis, and Royce D. Moore ; Lewis Research Center, Cleveland, Ohio
- Effect of casting geometry on mechanical properties of two nickel-base superalloys, James R. Johnston, Robert L. Dreshfield, and Henry E. Collins ; Lewis Research Center, Cleveland, Ohio
- Effect of coolant flow ejection on aerodynamic performance of low-aspect-ratio vanes : I--performance with coolant ejection holes plugged, Jeffrey E. Haas and Milton G. Kofskey ; Lewis Research Center, and U.S. Army Air Mobility R & D Laboratory, Cleveland, Ohio
- Effect of grazing flow on steady-state resistance of isolated square-edged orifices, by Thomas Rogers and Alan S. Hersh ; prepared by Hersh Acoustal Engineering, Chatsworth, Calif., for Lewis Research Center
- Effect of inlet temperature and pressure on emissions from a premixing gas turbine primary zone combustor/, Gerald Roffe ; prepared by General Applied Science Laboratories, inc. for Lewis Research Center
- Effects of forward velocity on turbulent jet mixing noise, prepared by Lockhead-Georgia Company, Marietta, Ga., for Lewis Research Center
- Effects of long-chord acoustically treated stator vanes on fan noise : II - effect of accoustical treatment, James H. Dittmar ... [and others] ; Lewis Research Center, Cleveland, Ohio
- Effects of motion on jet exhaust noise from aircraft, K. S. Chun, C. H. Berman, and S. J. Cowan ; prepared by Boeing Commercial Airplane Company, Seattle, Wash., for Lewis Research Center
- Effects of nozzle exit location and shape on propulsion-induced aerodynamic characteristics due to vectoring twin nozzles at Mach numbers from 0.4 ĚĄto 1.2, Francis J. Capone ; Langley Research Center, Hampton, Va
- Evaluation of an envelope-limiting device using simulation and flight test of a remotely piloted research vehicle, Kevin L. Petersen ; Dryden Flight Research Center, Edwards, Calif
- Evaluation of dispersion strengthened nickel-base alloy heat shields for space shuttle application, R. Johnson and D. H. Killpatrick
- Exhaust emission calibration of two J-58 afterburning turbojet engines at simulated high-altitude, supersonic flight conditions, James D. Holdeman ; Lewis Research Center, Cleveland
- Exhaust emissions from a premixing, prevaporizing flame tube using liquid jet A fuel, Cecil J. Marek and Leonidas C. Papathakos ; Lewis Research Center, Cleveland, Ohio
- Experimental aerodynamic characteristics for slender bodies with thin wings and tail at angles of attack from 0 ĚŠto 58 ĚŠand Mach from 0.6 to 2.0, Leland H. Jorgensen and Edgar R. Nelson ; Ames Research Center, Moffett Field, Calif
- Experimental and theoretical studies of subsonic fan noise, R. Mani and K. Bekofske
- Experimental investigation of a double-diffused MOS structure, H. C. Lin and J. L. Halsor ; prepared by Westinghouse Defense and Electronic Systems Center, Baltimore, Md, for Langley Research Center.
- Experimental investigation to validate use of cryogenic temperatures to achieve high Reynolds numbers in boattail pressure testing, David E. Reubush ; Langley Research Center, Hampton, Va
- Experimental study of transient dynamics of a flexible rotor, D. H. Hibner and D. F. Buono ; prepared by Pratt & Whitney Aircraft, East Hartford, Conn., for Lewis Research Center
- Exploratory study of transient unstart phenomena in a three-dimensional fixed-geometry scramjet engine, Allan R. Wieting ; Langley Research Center, Hampton, Va
- F-8C digital CCV flight control laws, Gary L. Hartmann, James A. Hauge, and Russell C. Hendrick ; prepared by Honeywell, Inc. for Langley Research Center
- Fabrication and surface characterization of composite refractory compounds suitable for thermionic converters, L. W. Swanson, J. T. Dickinson and D. R. McNeely
- Face-seal lubrication, II--theory of response to angular misalinement, Lawrence P. Ludwig and Gordon P. Allen ; Lewis Research Center, Cleveland, Ohio
- Fatigue-crack initiation and growth in notched 2024-T 3 specimens monitored by a video tape system, J. A. Sova, J. H. Crews, and R. J. Exton ; Langley Research Center, Hampton, Va
- Finite element computer program to analyze cracked orthotropic sheets, C. S. Chu ... [and others] ; prepared by Lockheed-Georgia Company, Marietta, Ga., for Langley Research Center
- Flowfield analysis for successive oblique shock wave-turbulent boundary layer interactions, Chen-Chih Sun and Morris E. Childs ; prepared by University of Washington, Seattle, Wash. for Ames Research Center
- Friction characteristics of 20 x 4.4, type VII, aircraft tires constructed with different tread rubber compounds, Robert C. Dreher and Thomas J. Yager ; Langley Research Center, Hampton Va
- Friction of iron lubricated with aliphatic and aromatic hydrocarbons and halogenated analogs, Donald H. Buckley ; Lewis Research Center, Cleveland, Ohio
- Fundamental analysis of the failure of polymer-based fiber reinforced composites, M. F. Kanninen ... [and others] ; prepared by Battelle, Columbus Laboratories, Columbus, Ohio for Ames Research Center
- Hover performance tests of full scale variable geometry rotors, James B. Rorke ; prepared by United Technologies Corporation, Stratford, Conn. for Langley Research Center and U.S. Army Air Mobility R & D Laboratory
- Influence of surface roughness and waviness on film thickness and pressure distribution in Elastohydrodynamic contacts, Lorac S. H. Chow and Herbert S. Cheng
- Infrared emission from the atmosphere above 200 km, Janet P. Simpson ; Ames Research Center, Moffett Field, Calif
- Inlet spillage drag tests and numerical flow-field analysis at subsonic and transonic speeds of a 1/8-scale, two-dimensional, external-compression, variable-geometry supersonic inlet configuration, J. E. Hawkins, F. P. Kirkland, and R. L. Turner ; prepared by General Dynamics Convair Aerospace Division, Fort Worth. Tex., for Ames Research Center
- Investigation of thermal fatigue in fiber composite materials, Abdel A. Fahmy and Thomas G. Cunningham ; prepared by North Carolina State University, Raleigh, N.C., for Langley Research Center
- Landing gear and cavity noise prediction, Donald B. Bliss and Richard E. Hayden ; prepared by Bolt, Beranek, and Newman Inc., Cambridge, Mass. for Langley Research Center
- Manual and automatic flight control during severe turbulence penetration, Donald E. Johnston, Richard H. Klein, and Roger H. Hob
- Measured opening characteristics of an electromagnetically opened diaphragm for the Langley expansion tunnel, John A. Moore ; Langley Research Center, Hampton, Va
- Measurement of lake ice thickness with a short-pulse radar system, Dale W. Cooper, Robert A. Mueller, and Ronald J. Schertler ; Lewis Research Center, Cleveland, Ohio
- Mechanical capacitor, James A. Kirk, Philip A. Studer, and Harold E. Evans ; Goddard Space Flight Center, Greenbelt, Md
- Meteorological adustment of yearly mean values for air pollutant concentration comparisons, Steven M. Sidik and Harold E. Neustadter ; Lewis Research Center, Cleveland, Ohio
- Multilayered models for electromagnetic reflection amplitudes, William I. Linlor ; Ames Research Center, Moffett Field, Calif
- Neural coding of high-frequency tones, Walton L. Howes ; Lewis Research Center, Cleveland, Ohio
- Noise measurements for a twin-engine commercial jet aircraft during 3 degree approaches and level flyovers, Earl C. Hastings, Jr., Robert E. Shanks, and Arnold W. Mueller ; Langley Research Center, Hampton, Va
- Noise reduction tests of large scale model externally blown flap using trailing-edge blowing and partial flap slot covering, David J. McKinzie, Jr., Robert J. Burns, and Jack M. Wagner ; Lewis Research Center, Cleveland, Ohio
- Noise suppression by an acoustically treated three-ring inlet on a TF-34 engine, Gene L. Minner, Richard G. Goldman, and Lawrence J. Heidelberg ; Lewis Research Center, Cleveland, Ohio
- Noise suppression with high Mach number inlets, Edward Lumsdaine, Jenn G. Cherng, and Ismail Tag ; prepared by the University of Tennessee, Knoxville, Tenn., for Langley Research Center
- On estimating gravity anomalies from gradiometer data, P. Argentiero and R. Garza-Robles ; Goddard Space Flight Center, Greenbelt, Md
- One-dimensional numerical analysis of the transient thermal response of multilayer insulative systems, Claud M. Pittman and Kay L. Brinkley ; Langley Research Center, Hampton, Va
- Overall and blade element performance of a 1.20 pressure ratio fan stage with rotor blades reset -7 ĚŠ/, George W. Lewis and George Kovich ; Lewis Research Center, Cleveland, Ohio
- Overall and blade element performance of a 1.20-pressure-ratio fan stage with rotor blades reset -5 ĚŠ/, George W. Lewis, Walter M. Osborn and Royce D. Moore ; Lewis Research Center, Cleveland, Ohio
- Performance of LI-1542 reusable surface insulation system in a hypersonic stream, L. Roane Hunt, John L. Shideler, and Irving Weinstein ; Langley Research Center, Hampton, Va
- Performance of a mullite reusable insulation system in a hypersonic stream, L. Roane Hunt ; Langley Research Center, Hampton, Va
- Perspective on the span-distributed-load concept for application to large cargo aircraft design, Allan H. Whitehead, Jr. ; Langley Research Center, Hampton, Va
- Plasma core reactor simulations using RF uranium seeded argon discharges, W. C. Roman ; prepared by United Technologies Reseach Center, East Hartfird, Conn. for Langley Research Center
- Prediction and verification of creep behavior in metallic materials and components for the space shuttle thermal protection system : summary report, John W. Davis and Bruce A. Cramer ; prepared by McDonnell Douglas Astronautics Company - East, St. Louis, Mo., for Langley Research Center
- Preliminary assessment of systems for deriving liquid and gaseous fuels from waste or grown organics, Robert W. Graham, Thaine W. Reynolds, and Yih-Yun Hsu ; Lewis Research Center, Cleveland
- Preliminary study of contaminant particulates around skylab, D. W. Schuerman and J. L. Weinberg ; prepared by State University of New York at Albany, Albany, N.Y. for George C. Marshall Space Flight Center
- Pressure distributions on a rectangular aspect-ratio-6, slotted supercritical airfoil wing with externally blown flaps, William G. Johnson, Jr. ; Langley Research Center, Hampton, Va
- Purging of multilayer insulation by gas diffusion, Irving E. Sumner and Charles M. Spuckler ; Lewis Research Center, Cleveland, Ohio
- Quantifying the benefits to the National economy from secondary applications of NASA technology : executive summary, prepared by Mathematica, Inc
- Quantifying the benefits to the National economy from secondary applications of NASA technology, prepared by Mathematica, Inc., Princeton, N.J
- Reduction of wind-tunnel wall interference by controlled wall flow, Samuel Bernstein and Robert G. Joppa
- Research in digital adaptive flight controllers, Howard Kaufman ; prepared by Rensselaer Polytechnic Institute, Troy, N.Y. for Langley Research Center
- Results of Skylab experiment T00-2, manual navigation sightings, Robert J. Randle ; Ames Research Center, Moffett Field, Calif
- Rolling-element fatigue life with two synthetic cycloaliphatic traction fluids, Stuart H. Loewenthal and Richard J. Parker ; Lewis Research Center and U.S. Army Air Mobility R & D Laboratory
- Selected fretting-wear-resistant coatings for titanium--6-percent-aluminum--4-percent-vanadium alloy, Robert C. Bill ; Lewis Research Center, Cleveland
- Selected methods for quantification of community exposure to aircraft noise, Philip M. Edge and Jimmy M. Cawthorn ; Langley Research Center, Hampton, Va
- Simplified solution for point contact deformation between two elastic solids, David E. Brewe and Bernard J. Hamrock ; Lewis Research Center and U.S. Army Air Mobility R & D Laboratory, Cleveland, Ohio
- Skin friction reduction by slot injection at mach 0.8, Victor Zakkay and Chi R. Wang ; prepared by New York University, Westbury, N.Y., for Langley Research Center
- Sound scattering by rigid oblate spheroids, with implication to pressure gradient microphones, Algirdas Maciulaitis, John M. Seiner, and Thomas D. Norum ; Langley Research Center, Hampton, Va
- Space shuttle electromagnetic environment experiment phase A; Definition study, Fred Haber ... [and others] ; prepared by the Moore School of Electrical Engineering, Philadelphia, Pa. for Goddard Space Flight Center
- Space shuttle pogo active controller design using frequency domain optimization, Robert C. Seidel, Carl F. Lorenzo, and Bruce Lehtinen ; Lewis Research Center, Cleveland, Ohio
- Spectral radiance measurements and calculated soot concentrations along the length of an experimental combustor, Carl T. Norgren and Robert D. Ingebo ; Lewis Research Center, Cleveland, Ohio
- Spectral reflectance and radiance characteristics of water pollutants, C. T. Wezernak, R. E. Turner, and D. R. Lyzenga ; prepared by Environmental Research Institute of Michigan, Ann Arbor, Mich. for Langley Research Center
- Strategies for estimating the marine geoid from altimeter data, P. Argentiero, W. D. Kahn, and R. Garza-Robles ; Goddard Space Flight Center, Greenbelt, Md
- Streakline flow visualization of discrete hole film cooling with holes inclined 30 ĚŠto surface, Raymond S. Colladay, Louis M. Russell, and Jan M. Lane ; Lewis Research Center, and U.S. Army Air Mobility R & D Laboratory
- Studies related to the development of the Viking 1975 labeled release experiment, Donald L. DeVincenzi and Paul H. Deal ; Ames Research Center, Moffett Field, Calif
- Study of a fail-safe abort system for an actively cooled hypersonic aircraft : volume I--technical summary, C. J. Pirrello and R. L. Herring; prepared by McDonnell Aircraft Company, St. Louis, Mo., for Langley Research Center.Center
- Study of flutter related computational procedures for minimum weight structural sizing of advanced aircraft, R. F. O'Connell, H. J. Hassig, and N. A. Radovcich
- Subjective response to combined noise and vibration during flight of a large twin-jet airplane, Sherman A. Clevenson ; Langley Research Center, Hampton, Va
- System tests with electric thruster beam and accelerator directly powered from laboratory solar arrays, John B. Stover ; Lewis Research Center, Cleveland, Ohio
- Test of a reduced-scale experimental model of a building solar heating-cooling system, David Namkoong ; Lewis Research Center, Cleveland, Ohio
- The effect of winglets on the static aerodynamic stability characteristics of a representative second generation jet transport model, Peter F. Jacobs and Stuart G. Flechner ; Langley Research Center, Hampton, Va
- The electron Boltzmann equation in a plasma generated by fission fragments, H. A. Hassan and Jerry E. Deese ; prepared by North Carolina State University, Raleigh, N.C
- The physiology and biochemistry of total body immobilization in animals : a compendium of research, Karen J. Dorchak and John E. Greenleaf ; Ames Research Center, Moffett Field, Calif
- The production of nitric oxide in the troposphere as a result of solid-rocket-motor afterburning, Roger B. Stewart and Richard I. Gomberg ; Langley Research Center, Hampton, Va
- Theoretical study of reactive and nonreactive turbulent coaxial jets, Roop N. Gupta and N. T. Wakelyn ; Langley Research Center, Hampton, Va
- Thrust performance of isolated two dimension suppressed plug nozzles with and without ejectors at mach numbers from 0 to 0.45, Douglas E. Harrington, James J. Schloemer, and Stanley A. Skebe ; Lewis Research Center, Cleveland, Ohio
- Transient effect of lubricant on elastohydrodynamic film thickness, K. L. Wang and H. S. Cheng ; prepared by Northwestern University, Evanston, Ill. for Lewis Research Center
- Transonic airfoil design using cartesian coordinates, Leland A. Carlson
- Two-layer thermal barrier coating for turbine airfoils - furnace and burner rig test results, Stephan Stecura ; Lewis Research Center, Cleveland, Ohio
- Vacuum ultraviolet spectra of uranium hexafluoride/argon mixtures, N. L. Krascella ; prepared by United Technologies Research Center, East Hartford, Conn. for Langley Research Center
- Wave theory of turbulence in compressible media, Creslaw P. Kentzer ; prepared by Purdue University, West Lafayette, Ind. for Langley Research Center
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<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.library.in.gov/resource/qBHgvw8V7kU/" typeof="PublicationEvent http://bibfra.me/vocab/lite/ProviderEvent"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.library.in.gov/resource/qBHgvw8V7kU/">Washington, U.S. National Aeronautics and Space Administration, Springfield, Va., for sale by the National Technical Information Service, 1976</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.library.in.gov/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.library.in.gov/">Indiana State Library</a></span></span></span></span></div>
