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Flight tests

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• Flight test results pertaining to the Space Shuttlecraft : a symposium held at Flight Research Center, Edwards, Calif., June 30, 1970. (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1970), by Flight Research Center (U.S.) (page images at HathiTrust)
• Description and operation of spacecraft in SERT I ion thrustor flight test / (Washington, D.C. : National Aeronautics and Space Administration ; Washington, D.C. : For sale by the Office of Technical Services, Department of Commerce [distributor], 1965), by Harold Gold and Lewis Research Center (page images at HathiTrust)
• Photographic investigation of liquid behavior on temperature and liquid-vapor sensors used in low-gravity environment / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1967), by James A. Berns, Ralph C. Nussle, Frederick C. Yeh, and Lewis Research Center (page images at HathiTrust)
• Measurement of flow angularity at supersonic and hypersonic speeds with the use of a conical probe / (Washington, [D.C.] : National Aeronautics and Space Administration, [1961]), by Frank E. Swalley, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Flight test of a 30-foot nominal diameter disk-gap-band parachute deployed at a Mach number of 1.56 and a dynamic pressure of 11.4 pounds per square foot / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1967), by Clinton V. Eckstrom, John S. Preisser, and Langley Research Center (page images at HathiTrust)
• Investigation of the performance characteristics of Doppler radar technique for aircraft collision hazard warning. (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1972), by Research Triangle Institute and Langley Research Center (page images at HathiTrust)
• Development and flight test of the Multichannel Ocean Colar Sensor (MOCS) / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1973), by P. G. White, Langley Research Center, and TRW Systems Group (page images at HathiTrust)
• Flight evaluation of splitter-plate effectiveness in reducing base drag at Mach numbers from 0.65 to 0.90 / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1967), by Edwin J. Saltzman, John Hintz, and Flight Research Center (U.S.) (page images at HathiTrust)
• XB-70 flight test data comparisons with simulation predictions of inlet unstart and buzz / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1970), by Arnold W. Martin, Warren D. Beaulieu, Flight Research Center (U.S.), and North American Rockwell Corporation (page images at HathiTrust)
• Flight test results of a trailing edge flap designed for direct-lift control / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1969), by Charles R. Taylor, Boeing Company, and Ames Research Center (page images at HathiTrust)
• Flight measurement of wall-pressure fluctuations and boundary-layer turbulence / (Washington [D.C.] : National Aeronautics and Space Administration, 1960), by Harold R. Mull, Joseph S. Algranti, and Lewis Research Center (page images at HathiTrust)
• A radar test target system / (Washington, [D.C.] : National Aeronautics and Space Administration, 1960), by James T. Rose, R. Donald Smith, and Langley Research Center (page images at HathiTrust)
• A flight investigation of an acceleration restrictor / (Washington, [D.C.] : National Aeronautics and Space Administration, 1960), by Arthur Assadourian, Donald L. Mallick, and Langley Research Center (page images at HathiTrust)
• An analysis of incremental horizontal-tail loads measured on a swept-wing bomber airplane in sideslip maneuvers / (Washington, [D.C.] : National Aeronautics and Space Administration, 1959), by William A. McGowan and Langley Research Center (page images at HathiTrust)
• A limited flight and wind-tunnel investigation of paddle spoilers as lateral controls / (Washington, [D.C.] : National Aeronautics and Space Administration, 1959), by Robert G. Mungall, William L. Alford, Harold I. Johnson, and Langley Research Center (page images at HathiTrust)
• Airplane and engine responses to abrupt throttle steps as determined from flight tests of eight jet-propelled airplanes / (Washington, [D.C.] : National Aeronautics and Space Administration, 1959), by Maurice D. White, Bernard A. Schlaff, and Ames Research Center (page images at HathiTrust)
• Two techniques for detecting boundary-layer transition in flight at supersonic speeds and at altitudes above 20,000 feet / (Washington, [D.C.] : National Aeronautics and Space Administration, 1959), by John G. McTigue, Gilbert Petty, John D. Overton, and Flight Research Center (U.S.) (page images at HathiTrust)
• Flight investigation of the lift and drag characteristics of a swept-wing, multijet, transport-type airplane / (Washington, [D.C.] : National Aeronautics and Space Administration, 1960), by Ronald Tambor and Flight Research Center (U.S.) (page images at HathiTrust)

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