Vortex flap flow reattachment line and subsonic longitudinal aerodynamic data on 50p0s to 74p0s delta wings on common fuselage
By: Neal T. Frink and Jarrett K. Huffman, Thomas D. Johnson, Jr
Contributors: Huffman, Jarrett K; Johnson, Thomas D; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
Series: NASA technical memorandum -- 84618
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1983
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 56
Subjects: Airplanes -- Wings, Canard; Leading edges (Aerodynamics); Flaps (Airplanes)
Notes: Distributed to depository libraries in microfiche

"December 1983"--Cover

Subject category 02

Includes bibliographical references