The Online Books Page

Online Books by

Acquilla S. Hill

Books from the extended shelves:

• Hill, Acquilla S.: Aerodynamic performance and pressure distributions for a NASA SC(2)-0714 airfoil tested in the Langley 0.3-meter transonic cryogenic tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), also by Renaldo V. Jenkins, Edward J. Ray, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust)
• Hill, Acquilla S.: Aerodynamics of a model of the HL-10 flight-test vehicle at Mach 0.35 to 1.80 (National Aeronautics and Space Administration, 1971), also by Charles L. Ladson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Hill, Acquilla S.: Calibration of the 13- by 13-inch adaptive wall test section for the Langley O.3-meter transonic cryogenic tunnel (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Raymond E. Mineck and Langley Research Center (page images at HathiTrust)
• Hill, Acquilla S.: CAST-10-2/DOA 2 Airfoil Studies Workshop results : proceedings of a workshop (NASA, Office of Management, Scientific and Technical Information Division, 1989), also by CAST-10-2/DOA 2 Airfoil Studies Workshop (1988 : NASA Langley Research Center) and Edward J. Ray (page images at HathiTrust)
• Hill, Acquilla S.: High Reynolds number tests of a NASA SC(3)-0712(B) airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by William G. Johnson, Otto Eichmann, and Langley Research Center (page images at HathiTrust)
• Hill, Acquilla S.: Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by William G. Johnson and Langley Research Center (page images at HathiTrust)
• Hill, Acquilla S.: Pressure distributions from high Reynolds number tests of a NASA SC(3)-0712(B) airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by William G. Johnson, Otto Eichmann, and Langley Research Center (page images at HathiTrust)

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