- Additional Authors
- Description
- 1 online resource (144 pages) : illustrations.
- Series Statement
- NASA technical paper ; 1552
- Uniform Title
- NASA technical paper ; 1552.
- Subject
- Note
- Title from title screen (viewed Sept. 22, 2014).
- "December 1979."
- "Performing organization, NASA Langley Research Center"--Technical report documentation page.
- Bibliography (note)
- Includes bibliographical references (pages 20-22).
- Funding (note)
- Sponsored by National Aeronautics and Space Administration
- Call Number
- GPO Internet NAS 1.60:1552
- OCLC
- marcive761863635
- Author
Penland, Jim A., author.
- Title
Aerodynamic characteristics of a hypersonic research airplane concept having a 70̊ swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0 / Jim A. Penland, James B. Hallissy, and James L. Dillon.
- Publisher
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1979.
- Type of Content
text
- Type of Medium
computer
- Type of Carrier
online resource
- Series
NASA technical paper ; 1552
NASA technical paper ; 1552.
- Bibliography
Includes bibliographical references (pages 20-22).
- Funding
Sponsored by National Aeronautics and Space Administration 505-11-33-01
L-13158
- Connect to:
- Added Author
Hallissy, James B., author.
Dillon, James L., author.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, issuing body.
Langley Research Center, author.
- Other Form:
Print version: Penland, Jim A. Aerodynamic characteristics of a hypersonic research airplane concept having a 70̊ swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0 (OCoLC)8216364
- Gpo Item No.
0830-H-15 (online)
- Sudoc No.
NAS 1.60:1552