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U.S. Army Air Mobility Research and Development Laboratory

Books from the extended shelves:

U.S. Army Air Mobility Research and Development Laboratory: Acoustic characteristics of a large-scale wind-tunnel model of a jet flap aircraft (National Aeronautics and Space Administration ;, 1975), also by Michael D. Falarski, Kiyoshi Aoyagi, Thomas N. Aiken, and Ames Research Center (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Aeorelastic analysis for helicopter rotor blades with time-variable, nonlinear structural twist and multiple structural redundancy-mathematical derivation and program user's manual (National Aeronautics and Space Administration ;, 1976), also by Richard L. Bielawa, United Technologies Research Center, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Aerodynamic characteristics of a 1/6-scale powered model of the rotor systems research aircraft (National Aeronautics and Space Administration ;, 1977), also by Raymond E. Mineck, Carl E. Freeman, and United States National Aeronautics and Space Administration (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Aerodynamic characteristics of a large-scale model a lift fan mounted in a 5-percent-thick triangular wing, including the effects of BLC on the lift-fan inlet (National Aeronautics and Space Administration, 1970), also by Brent K. Hodder, Leo P. Hall, Jerry V. Kirk, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Analysis of dynamic capacity of low-contact-ratio spur gears using Lundberg-Palmgren theory (National Aeronautics and Space Administration ;, 1975), also by John J. Coy, Erwin V. Zaretsky, Dennis P. Townsend, and Lewis Research Center (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Analysis of helicopter rotor blade torsional oscillations due to stall (National Aeronautics and Space Administration ;, 1975), also by Peter Crimi, Langley Research Center, and Avco Corporation. Systems Division (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Analytical modeling requirements for tilting proprotor aircraft dynamics (National Aeronautics and Space Administration ;, 1975), also by Wayne Johnson and Ames Research Center (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Cold-air performance of a tip turbine designed to drive a lift fan : II, partial admission (National Aeronautics and Space Administration ;, 1977), also by Jeffrey E. Haas, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: A comparison of optimal and noise-abatement trajectories of a tilt-rotor aircraft (National Aeronautics and Space Administration ;, 1972), also by Frederic H. Schmitz, United States National Aeronautics and Space Administration, Ames Research Center, and Boeing Company (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Comparison of three methods for calculation of helicopter rotor blade loading and stresses due to stall (National Aeronautics and Space Administration ;, 1974), also by Wayne Johnson and Ames Research Center (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Correlation of elastohydrodynamic film thickness measurements for fluorocarbon, type II ester, and polyphenyl ether lubricants (National Aeronautics and Space Administration ;, 1974), also by Stuart H. Loewenthal, Erwin V. Zaretsky, Richard J. Parker, and Lewis Research Center (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Design of experiments for measuring heat-transfer coefficients with a lumped-parameter calorimeter (National Aeronautics and Space Administration ;, 1975), also by G. James VanFossen and Lewis Research Center (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Determination of rotor harmonic blade loads from acoustic measurements (National Aeronautics and Space Administration ;, 1975), also by Peter K. Kasper, Langley Research Center, and Wyle Laboratories (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Dynamics of tilting proprotor aircraft in cruise flight (National Aeronautics and Space Administration ;, 1974), also by Wayne Johnson and Ames Research Center (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Effect of carbide size, area, and density on rolling-element fatigue (National Aeronautics and Space Administration ;, 1972), also by James L. Chevalier, Erwin V. Zaretsky, and Lewis Research Center (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Effect of coolant flow ejection on aerodynamic performance of low-aspect-ratio vanes : I--performance with coolant ejection holes plugged (U.S. National Aeronautics and Space Administration ;, 1976), also by Jeffrey E. Haas, Milton G. Kofskey, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Elastohydrodynamic analysis using a power law pressure-viscosity relation (National Aeronautics and Space Administration ;, 1973), also by Stuart H. Loewenthal, Erwin V. Zaretsky, and Lewis Research Center (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Elastohydrodynamic film thickness formula based on X-ray measurements with a synthetic paraffinic oil (National Aeronautics and Space Administration ;, 1973), also by Stuart H. Loewenthal, Erwin V. Zaretsky, Richard J. Parker, and Lewis Research Center (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Exhaust pollutant emissions from swirl-can combustor module arrays at parametric test conditions (National Aeronautics and Space Administration ;, 1975), also by Edward J. Mularz, Peter W. Verbulecz, Jerrold D. Wear, and Lewis Research Center (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Experimental dynamic stiffness and damping of externally pressurized gas-lubricated journal bearings (National Aeronautics and Space Administration ;, 1976), also by David P. Fleming, Robert E. Cunningham, William J. Thayer, and Lewis Research Center (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Experimental evaluation of compliant surfaces at low speeds (National Aeronautics and Space Administration ;, 1974), also by Kenneth W. McAlister, Tom M. Wynn, and Ames Research Center (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Experimental flow coefficients of a full-coverage film-cooled-vane chamber (National Aeronautics and Space Administration., 1977), also by Peter L. Meitner, Steven A. Hippensteele, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: An experimental investigation of end treatments for nonreturn wind tunnels (U.S. National Aeronautics and Space Administration ;, 1976), also by William T. Eckert, J. E. Piazza, Kenneth W. Mort, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: External fins and ejector action for reducing the infrared emission of engine exhaust ducting (National Aeronautics and Space Administration ;, 1975), also by G. James VanFossen and Lewis Research Center (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Flapping response characteristics of hingeless rotor blades by a generalized harmonic balance method (National Aeronautics and Space Administration ;, 1975), also by D. A. Peters, Robert A. Ormiston, and Ames Research Center (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Flow characteristics of various swirl-can module designs (National Aeronautics and Space Administration ;, 1975), also by Edward J. Mularz and Lewis Research Center (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: FORTRAN program for predicting off-design performance of centrifugal compressors (National Aeronautics and Space Administration ;, 1973), also by Michael R. Galvas and Lewis Research Center (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Fretting of nickel-chromium-aluminum alloys at temperatures to 816 ̊C (National Aeronautics and Space Administration ;, 1974), also by Robert C. Bill and Lewis Research Center (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Fretting of titanium at temperatures to 650 ̊C in air (National Aeronautics and Space Administration ;, 1975), also by Robert C. Bill and Lewis Research Center (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Friction and wear of carbon-graphite materials for high-energy brakes (National Aeronautics and Space Administration ;, 1975), also by Robert C. Bill and Lewis Research Center (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Full-scale wind-tunnel tests of a small unpowered jet aircraft with a T-Tail (National Aeronautics and Space Administration ;, 1971), also by Paul T. Soderman, Thomas N. Aiken, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Hot hardness characteristics of ausformed AISI M-50, Matrix II, WD-65, modified AISI 440-C, and Super Nitralloy (National Aeronautics and Space Administration ;, 1973), also by James L. Chevalier, Erwin V. Zaretsky, Marshall W. Dietrich, and Lewis Research Center (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Hover performance tests of full scale variable geometry rotors (U.S. National Aeronautics and Space Administration ;, 1976), also by James B. Rorke, United States National Aeronautics and Space Administration, Langley Research Center, and United Technologies Corporation (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Kinematic stability of roller pairs in free-rolling contact (National Aeronautics and Space Administration ;, 1976), also by M. Savage, Stuart H. Loewenthal, and Lewis Research Center (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Landing approach evaluation of an integrated CRT display for general aviation aircraft (National Aeronautics and Space Administration ;, 1974), also by Peter D. Talbot, Glen W. Stinnett, and Ames Research Center (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Life analysis of helical gear sets using Lundberg-Palmgren theory (National Aeronautics and Space Administration ;, 1975), also by John J. Coy, Erwin V. Zaretsky, and Lewis Research Center (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Lifting-surface theory for calculating the loading induced on a wing by a flap (National Aeronautics and Space Administration ;, 1972), also by Wayne Johnson, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Load and stability measurements on a soft-inplane rotor system incorparting elsatomeric lead-lag dampers (National Aeronautics and Space Administration ;, 1977), also by William H. Weller and United States National Aeronautics and Space Administration (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Measurements of liner cooling effectiveness within a full-scale double-annular ram-induction combustor (National Aeronautics and Space Administration ;, 1974), also by Edward J. Mularz and Donald F. Schultz (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: NASA TN D-6321 (National Aeronautics and Space Administration ;, 1971), also by William J. McCroskey, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
U.S. Army Air Mobility Research and Development Laboratory: NASA TN D-6709 (National Aeronautics and Space Administration :, 1972), also by Robert E. King, Gregory W. Condon, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
U.S. Army Air Mobility Research and Development Laboratory: NASA TN D-7881 (National Aeronautics and Space Administration ;, 1975), also by Jeffrey E. Haas, Milton G. Kofskey, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
U.S. Army Air Mobility Research and Development Laboratory: Nonlinear equations of motion for the elastic bending and torsion of twisted nonuniform rotor blades (National Aeronautics and Space Administration ;, 1974), also by Dewey H. Hodges, E. H. Dowell, and Ames Research Center (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Oxidation at through-hole defects in fused slurry silicide coated columbian [i.e. columbium] alloys FS-85 and Cb-752 (National Aeronautics and Space Administration ;, 1973), also by Stanley R. Levine and Lewis Research Center (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Performance of coated columbium and tantalum alloys in plasma arc reentry simulation tests (National Aeronautics and Space Administration ;, 1974), also by Stanley R. Levine, John P. Merutka, and Lewis Research Center (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Pitting fatigue characteristics of AISI M-50 and Super Nitralloy spur gears (National Aeronautics and Space Administration ;, 1973), also by Dennis P. Townsend, Erwin V. Zaretsky, James L. Chevalier, and Lewis Research Center (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Properties of solid polymer electrolyte fluorocarbon film (National Aeronautics and Space Administration ;, 1973), also by William B. Alston and Lewis Research Center (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Role of plastic deformation in wear of copper and copper-10-percent-aluminum alloy in cryogenic fuels (National Aeronautics and Space Administration ;, 1973), also by Robert C. Bill, Donald W. Wisander, and Lewis Research Center (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Rolling-element fatigue life with two synthetic cycloaliphatic traction fluids (U.S. National Aeronautics and Space Administration ;, 1976), also by Stuart H. Loewenthal, Richard J. Parker, and Lewis Research Center (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Short-term hot-hardness characteristics of five case hardened steels (National Aeronautics and Space Administration ;, 1975), also by Neil E. Anderson, Erwin V. Zaretsky, and Lewis Research Center (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Short-term hot hardness characteristics of rolling-element steels (National Aeronautics and Space Administration ;, 1972), also by James L. Chevalier, Erwin V. Zaretsky, Marshall W. Dietrich, and Lewis Research Center (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Simplified solution for point contact deformation between two elastic solids (U.S. National Aeronautics and Space Administration ;, 1976), also by David E. Brewe, Bernard J. Hamrock, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Streakline flow visualization of discrete hole film cooling with holes inclined 30 ̊to surface (U.S. National Aeronautics and Space Administration ;, 1976), also by Raymond S. Colladay, Jan M. Lane, Louis M. Russell, and Lewis Research Center (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Summary of propeller design procedures and data ([Fort Eustis, Virginia] : [Eustis Directorate, U.S. Army Air Mobility Research and Development Laboratory], [1973], 1973), also by Henry V. Borst and Henry V. Borst & Associates (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Surface heat-transfer coefficients of pin-finned cylinders (National Aeronautics and Space Administration ;, 1975), also by G. James VanFossen and Lewis Research Center (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Surface recrystallization theory of the wear of copper in liquid methane (National Aeronautics and Space Administration ;, 1974), also by Robert C. Bill, Wisander Donald W., and Lewis Research Center (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Three-dimensional elastic stress and displacement analysis of tensile fracture specimens containing cracks (National Aeronautics and Space Administration ;, 1973), also by John P. Gyekenyesi, Jon Kring, Alexander Mendelson, and Lewis Research Center (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: Turbine for a low-cost turbojet engine (National Aeronautics and Space Administration ;, 1974), also by Milton G. Kofskey and Lewis Research Center (page images at HathiTrust)
U.S. Army Air Mobility Research and Development Laboratory: A wind-tunnel investigation of an unpowered helicopter fuselage model with a V-type empennage (National Aeronautics and Space Administration ;, 1977), also by Carl E. Freeman, William T. Yeager, and United States National Aeronautics and Space Administration (page images at HathiTrust)

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