U.S. Army Air Mobility Research and Development Laboratory
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The organization U.S. Army Air Mobility Research and Development Laboratory represents an institution, an association, or corporate body that is associated with resources found in Indiana State Library.
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U.S. Army Air Mobility Research and Development Laboratory
Resource Information
The organization U.S. Army Air Mobility Research and Development Laboratory represents an institution, an association, or corporate body that is associated with resources found in Indiana State Library.
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- U.S. Army Air Mobility Research and Development Laboratory
- Authority link
- (EG-IN)980122
40 Items by the Organization U.S. Army Air Mobility Research and Development Laboratory
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- A method for predicting helicopter hub drag : final report
- A wind-tunnel investigation of an unpowered helicopter fuselage model with a V-type empennage
- Advanced scavenge systems for an integrated engine inlet particle separator : final report for period 21 March 1975-21 March 1977
- Aeorelastic analysis for helicopter rotor blades with time-variable, nonlinear structural twist and multiple structural redundancy-mathematical derivation and program user's manual
- Aerodynamic characteristics of a 1/6-scale powered model of the rotor systems research aircraft
- Aerodynamic design guidelines and computer program for estimation of subsonic wind tunnel performance
- Aeroelastic rotor stability analysis
- An analytical investigation of the effects of increased installed horsepower on helicopter agility in the nap-of-the-earth environment
- An experimental investigation of end treatments for nonreturn wind tunnels
- Axial-centrifugal compressor program, evaluation of ausformed bearings : final report for period 1 August 1972 - 15 June 1975
- CH-54 operational statistics : final report
- Cold-air performance of a tip turbine designed to drive a lift fan : I, baseline performance
- Cold-air performance of a tip turbine designed to drive a lift fan : II, partical admission
- Design, fabrication, and testing of an adavnce composite AH-1G tail section (tail boom/vertical fin) : final report for period July 1973-February 1976
- Effect of coolant flow ejection on aerodynamic performance of low-aspect-ratio vanes : I--performance with coolant ejection holes plugged
- Experimental dynamic stiffness and damping of externally pressurized gas-lubricated journal bearings
- Experimental flow coefficients of a full-coverage film-cooled-vane chamber
- Field evaluation of UH-1H helicopter inspection systems project inspect, phase II : final report for period 1 May 1974-31 May 1976
- Flight test of a composite multi-tubular spar main rotor blade on the AH-1G helicopter : final report for period June 1974 - January 1977
- Helicopter reliability growth evaluation
- Helicopter transmission vibration and noise reduction program : final report for period May 1974-February 1977
- High-survivable transmission system : final report for period January 1974-August 1975
- Hover performance tests of full scale variable geometry rotors
- Integrated accessory systems for small gas turbine engines
- Limitations of the CH-47 helicopter in performing terrain flying with external loads
- Limitations of the Uttas helicopter in performing terrain flying with external loads : final report for period July 1976-Apr. 1977
- Load and stability measurements on a soft-inplane rotor system incorporating elastomeric lead-lag dampers
- MM&T, pultruded composite structural elements
- Ottawa spray rig tests of an ice protection system applied to the UH1H helicopter : final report for period January 1976-May 1976
- Preliminary design study of an integrated tail rotor servo power module : final report
- Production suitability of an electroform conductive wax process for the manufacture of fluidic systems : phase II
- Production suitability of an electroform conductive-wax process for the manufactures of fluidic systems : final report for period March 1976 - October 1976
- Refinement of casting techniques for small air-cooled turbine blades : phase 1 : final report for period September 1973-December 1975
- Rolling-element fatigue life with two synthetic cycloaliphatic traction fluids
- Simplified solution for point contact deformation between two elastic solids
- Small hardware design for ease of maintenance and inspection : final report for period July 1973 - March 1976
- Streakline flow visualization of discrete hole film cooling with holes inclined 30 ĚŠto surface
- Transmission condition assessment : final report
- Validation of the rotorcraft flight simulation program (C81) for articulated rotor helicopters through correlation with flight data : final report for period June 1974-Jan. 1976
- Wear-indicating rod end bearing : advance report for period June 1975-May 1976
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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/v_ivKlt3coY/" typeof="Organization http://bibfra.me/vocab/lite/Organization"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.library.in.gov/resource/v_ivKlt3coY/">U.S. Army Air Mobility Research and Development Laboratory</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>
