Experimental determination of flow-interference effects of wing-mounted two-dimensional, full-capture propulsion nacelles in close proximity to a vehicle body at a Mach number of 6
By: Walter A. Vahl
Contributors: Langley Research Center; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
Series: NASA technical memorandum -- 83287
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1982
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 33
Subjects: Aerodynamics; Airplanes -- Nacelles -- Testing; Aerodynamics, Hypersonic -- Testing
Notes: "May 1982"--Cover

Subject category 02

Includes bibliographical references