Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0
By: Jim A. Penland, James B. Hallissy, and James L. Dillon
Contributors: Hallissy, James B., author; Dillon, James L., author; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch; Langley Research Center
Series: NASA technical paper -- 1552; NASA technical paper -- 1552.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch
Published: 1979
Place of publication: Washington, D.C
Language: eng
Number of pages: 144
Subjects: Aerodynamics; Aerodynamic characteristics; Computational fluid dynamics; Delta wings; Hypersonic aircraft; Wind tunnel tests
Notes: Title from title screen (viewed Sept. 22, 2014).

"December 1979."

"Performing organization, NASA Langley Research Center"--Technical report documentation page.

Includes bibliographical references (pages 20-22).

Sponsored by National Aeronautics and Space Administration 505-11-33-01

L-13158