Effects of inlet distortion on a static pressure probe mounted on the engine hub in an F-15 airplane
By: Donald L. Hughes, Lawrence P. Myers, and Karen G. Mackall.
Contributors: Myers, Lawrence P.; Mackall, Karen G.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Series: NASA technical paper -- 2411.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch
Published: 1985
Place of publication: Washington, D.C
Language: eng
Format: Microform
Subjects: Static pressure probes -- Testing.; Airplanes -- Turbojet engines -- Air intakes.; Eagle (Jet fighter plane)
Notes: Includes bibliographical references (p. 6).

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1985] 1 microfiche.