Experimental study of acoustic loads on upper-surface-blown STOL airplane configuration
By: Conrad M. Willis and James A. Schoenster
Contributors: Schoenster, James A; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch; Langley Research Center
Series: NASA technical paper -- 1577
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1979
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 54
Subjects: Airplanes -- Testing; Jet flaps (Airplanes) -- Testing; Airplanes -- Fuselage -- Testing; Acoustical engineering
Notes: "December 1979"--Cover

"Langley Research Center."

Includes bibliographical references