Aerodynamics, Hypersonic
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The concept Aerodynamics, Hypersonic represents the subject, aboutness, idea or notion of resources found in Indiana State Library.
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Aerodynamics, Hypersonic
Resource Information
The concept Aerodynamics, Hypersonic represents the subject, aboutness, idea or notion of resources found in Indiana State Library.
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- Aerodynamics, Hypersonic
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- (EG-IN)1251821
116 Items that share the Concept Aerodynamics, Hypersonic
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- Wall-temperature effects on the aerodynamics of a hydrogen-fueled transport concept in Mach 8 blowdown and shock tunnels
- A High angle of attack inviscid shuttle orbiter computation
- A Hot dynamic seal rig for measuring hypersonic engine seal durability and flow performance
- A high-frequency servosystem for fuel control in hypersonic engines
- A modified T-value method for selection of strain gages for measuring loads on a low aspect ratio wing
- A preliminary assessment of the impact of 2-D exhaust-nozzle geometry on the cruise range of a hypersonic aircraft with top-mounted ramjet propulsion
- A study of viscous interaction effects on hypersonic waveriders
- A test fixture for measuring high-temperature hypersonic-engine seal performance
- Addition of equilibrium air to an upwind Navier-Stokes code and other first steps toward a more generalized flow solver
- Advanced computational techniques for hypersonic propulsion
- Aerodynamic analysis of hypersonic waverider aircraft
- Aerodynamic characteristics at Mach number 0.2 of a wing-body concept for a hypersonic research airplane
- Aerodynamic characteristics of a vane flow angularity sensor system capable of measuring flightpath accelerations for the mach number range from 0.40 to 2.54
- Aerodynamic characteristics of two single-stage-to-orbit vehicles at Mach 20.3
- Aerodynamic characteristics, including effect of body shape, of a Mach 6 aircraft concept
- Aerodynamic heating rate distributions induced by trailing edge controls on hypersonic aircraft configurations at Mach 8
- Aerodynamic pressure and heating-rate distributions in tile gaps around chine regions with pressure gradients at a Mach number of 6.6
- Aerodynamic pressures and heating rates on surfaces between split elevons at Mach 6.6
- Aerothermal loads analysis for high speed flow over a quilted surface configuration
- An approximate viscous shock layer technique for calculating chemically reacting hypersonic flows about blunt-nosed bodies
- An engineering method for interactive inviscid-boundary layers
- An explicit upwind algorithm for solving the parabolized Navier-Stokes equations
- An upwind-biased space marching algorithm for supersonic viscous flow
- Analytical and experimental investigations of the oblique detonation wave engine concept
- Assessment of a flow-through balance for hypersonic wind tunnel models with scramjet exhaust flow simulation
- Combined LAURA-UPS solution procedure for chemically-reacting flows
- Comparison of measured and calculated temperatures for a Mach 8 hypersonic wing test structure
- Compendium of NASA Langley reports on hypersonic aerodynamics
- Computation of H2/air reacting flowfields in drag-reduction external combustion
- Computational analysis of hypersonic flows past elliptic-cone waveriders
- Computational parametric study of sidewall-compression scramjet inlet performance at mach 10
- Conservation equations and physical models for hypersonic air flows in thermal and chemical equilibrium
- Development of a 3-D upwind PNS code for chemically reacting hypersonic flowfields
- Development of a computer code for calculating the steady super/hypersonic inviscid flow around real configurations : volume I-computational technique
- Development of a computer code for calculating the steady super/hypersonic inviscid flow around real configurations : volume II - code description
- Development of a thermal and structural model for a NASTRAN finite-element analysis of a hypersonic wing test structure
- Development of braided rope seals for hypersonic engine applications : flow modeling
- Dynamic interactions between hypersonic vehicle aerodynamics and propulsion system performance : final report to Aircraft Guidance and Controls Branch, Guidance and Control Division ...
- Effect of modifications on aerodynamic characteristics of a single-stage-to-orbit vehicle at Mach 5.9
- Effects of Görtler vortices, wall cooling and gas dissociation on the Rayleigh instability in a hypersonic boundary layer
- Effects of external stores on the aerodynamic characteristics of a 60 ĚŠDelta-wing fighter model at Mach 1.60 to 2.87
- Effects of nose bluntness and shock-shock interactions on blunt bodies in viscous hypersonic flows : progress report for the period ended December 31, 1989
- Evaluation of a technique to generate artificially thickened boundary layers in supersonic and hypersonic flows
- Evaluation of an innovative high temperature ceramic wafer seal for hypersonic engine applications
- Experimental investigation of generic three-dimensional sidewall-compression scramjet inlets at Mach 6 in tetrafluoromethane
- Experimental investigation of hypersonic aerodynamics : research report
- Experimental investigation of nozzle/plume aerodynamics at hypersonic speeds : periodic progress research report for cooperative agreement NCC2-487 for the period Feburary 1, 1992 - November 30, 1992
- Experimental research of the aerodynamics of nozzles and plumes at hypersonic speeds
- Exploratory investigation of the aerodynamic characteristics of a biwing vehicle at Mach 20.3
- Exploratory study of transient unstart phenomena in a three-dimensional fixed-geometry scramjet engine
- Flow analysis and design optimization methods for nozzle after body of a hypersonic vehicle
- Fluctuating pressures measured beneath a high-temperature, turbulent boundary layer on a flat plate at a Mach number of 5
- Generic hypersonic vehicle performance model : interim task report for NASA grant NAG-1-1341
- Ground effects on the low-speed aerodynamics of a powered, generic hypersonic configuration
- H-P adaptive methods for finite element analysis of aerothermal loads in high-speed flows
- Heat transfer characteristics of hypersonic waveriders with an emphasis on the leading edge effects
- Heat transfer distributions induced by elevon deflections on swept wings and adjacent surfaces at Mach 6
- High speed aeronautics : hearing before the Subcommittee on Transportation, Aviation, and Materials of the Committee on Science and Technology, U.S. House of Representatives, Ninety-ninth Congress, first session, July 24, 1985
- High-resolution shock-capturing schemes for inviscid and viscous hypersonic flows
- Hypersonic aerodynamic coefficients and convection flow estimation in a Hermes type project
- Hypersonic airframe structures technology needs and flight test requirements
- Hypersonic characteristics of an advanced aerospace plane at Mach 20.3
- Hypersonic flow analysis : final report for the period, September 1, 1986 - August 31, 1987
- Hypersonic flows as related to the national aerospace plane : semi-annual research report for cooperative agreement no. NCC2-452 for the period September 1, 1991 - May 31, 1992
- Hypersonic flows as related to the national aerospace plane : semi-annual research report for cooperative agreement no.: NCC2-452 for the period August 1, 1990 - February 28, 1991
- Hypersonic turbulent wall boundary layer computations
- Hypersonic vehicle control law development using H[infinity symbol] and [mu]-synthesis
- Improved tangent-cone method for the Aerodynamic Preliminary Analysis System (APAS) version of the hypersonic arbitrary-body program
- Instrumentation for hypersonic aerodynamics research with tethered satellites : final report fo the period January 1, 1990 to January 15, 1992
- Investigation of effect of propulsion system installation and operation on aerodynamics of an airbreathing hypersonic airplane at Mach O.3 to 1.2
- Investigation of nose bluntness and angle of attack effects on slender bodies in viscous hypertension flows
- Laminar heat-transfer distributions on biconics at incidence in hypersonic-hypervelocity flows
- Loading tests of a wing structure for a hypersonic aircraft
- Longitudinal aerodynamic characteristics at Mach 0.60 to 2.86 of a fighter configuration with strut braced wing
- Longitudinal aerodynamic characteristics at Mach numbers from 1.60 to 2.86 for a spanmissile with three wing planforms
- Longitudinal aerodynamic characteristics of a fighter model with a close-coupled canard at Mach numbers from 0.40 to 1.20
- Mach 4 free-jet tunnel-starting experiments for a hypersonic research engine model causing high blockage
- Maximum lift/drag ratio of flat plates with bluntness and skin friction at hypersonic speeds
- Measured and predicted shock shapes and aerodynamic coefficients for blunted cones at incidence in air at Mach 5.9
- Measured and predicted shock shapes and aerodynamic coefficients for blunted cones at incidence in helium at Mach 20.3
- Measured pressure distributions, aerodynamic coefficients, and shock shapes on blunt bodies at incidence in hypersonic air and CF4
- Modification to the Langley 8-foot high temperature tunnel for hypersonic propulsion testing
- Multigrid for hypersonic inviscid flows
- Multigrid for hypersonic viscous two-and three-dimensional flows
- Nonlinear development and secondary instability of Görtler vortices in hypersonic flows
- Nonlinear instability of hypersonic flow past a wedge
- Nonlinear potential analysis techniques for supersonic/hypersonic aerodynamic design
- Nonparallel instability of supersonic and hypersonic boundary layers
- Numerical computation of space shuttle orbiter flow field : semi-annual status report, April 1, 1984 - September 30, 1984
- Numerical procedure for three-dimensional hypersonic viscous flow over aerobrake configuration
- Numerical simulation of the hypersonic flow around lifting vehicles
- Numerical study of unsteady viscous hypersonic blunt body flows with an impinging shock
- Particle kinetic simulation of high altitude hypervelocity flight
- Particle kinetic simulation of high altitude hypervelocity flight : periodic research report, cooperative agreement NCC2-582 for the period January 1, 1993 - August 31, 1993
- Perspectives on hypersonic viscous nad nonequilibrium flow research
- Pitot survey of exhaust flow field of a 2-D scramjet nozzle at Mach 6 with air or freon and argon used for exhaust simulation
- Power-on performance predictions for a complete generic hypersonic vehicle configuration
- Progress with multigrid schemes for hypersonic flow problems
- Radiation transfer regimes in hypersonic flight
- Real-time aerodynamic heating and surface temperature calculations for hypersonic flight simulation
- Reynolds number influences in aeronautics
- Secondary instability of high-speed flows and the influence of wall cooling and suction
- Shock tunnel studies for scramjet phenomena, supplement 6
- Simplified curved fits for the thermodynamic properties of equilibrium air
- Simulation of real-gas effects on pressure distributions for aeroassist flight experiment vehicle and comparison with prediction
- Space shuttle hypersonic aerodynamic and aerothermodynamic flight research and the comparison to ground test results
- Stagnation-point heat-transfer rate predictions at aeroassist flight conditions
- Studies of aerothermal loads generated in regions of shock/shock interaction in hypersonic flow
- Studies of shock/shock interaction on smooth and transpiration-cooled hemispherical nosetips in hypersonic flow
- The Hypersonic revolution : eight case studies in the history of hypersonic technology
- The effect of exhaust plume/afterbody interaction on installed scramjet performance
- Thermal-structural design study of an airframe-integrated scramjet : summary report
- Turbulence modeling for hypersonic flight
- Two- and three-dimensional viscous computations of a hypersonic inlet flow
- Upgrading of NASA-Ames high-energy hypersonic facilities : a study
- Viscous computations of cold air/airflow around scramjet nozzle afterbody
- Viscous flow simulations of internal store carriage and separation : final report for the period ended May 15, 1991
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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/eCtWFxdRQC0/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.library.in.gov/resource/eCtWFxdRQC0/">Aerodynamics, Hypersonic</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>
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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/eCtWFxdRQC0/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.library.in.gov/resource/eCtWFxdRQC0/">Aerodynamics, Hypersonic</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>
