Development of flow distortions in a full-scale nacelle inlet at mach numbers 0.63 and 1.6 to 2.0 - Piercy, Thomas G.; Chiccine, Bruce G.; Lewis Flight Propulsion Laboratory; United States. National Adviosry Committee for Aeronautics; United States. National Advisory Committee for Aeronautics (Washington, D.C. : National Advisory Committee for Aeronautics, 1956)
"October 22, 1955."
Includes bibliographical references (p. 16-17).
Mode of access: Internet.
Keywords: Mach number; Aerodynamics, Supersonic; Air ducts; Airplanes -- Wings