2 options
Effect of forebody strakes on the aerodynamic characteristics in pitch and sideslip of a hypersonic airplane configuration at Mach numbers of 1.41, 2.01, and 6.86 / by Cornelius Driver.
- Format:
- Book
- Government document
- Author/Creator:
- Driver, Cornelius, author.
- Series:
- NASA technical memorandum ; X-116.
- NASA/TM; X-116
- Language:
- English
- Subjects (All):
- Aerodynamics.
- Aerodynamic measurements.
- Mach number.
- Hypersonic planes.
- Wind tunnel testing.
- Shells (Engineering).
- Noses (Aircraft).
- aerodynamics.
- shell structures.
- Physical Description:
- 1 online resource (47 pages) : illustrations.
- Place of Publication:
- Washington : National Aeronautics and Space Administration, September 1959.
- Notes:
- "September 1959"--Cover.
- Includes bibliographical references (page 6).
- Description based on online resource; title from PDF cover, (NASA, viewed on May 26, 2022).
- Other Format:
- Print version: Driver, Cornelius. Effect of forebody strakes on the aerodynamic characteristics in pitch and sideslip of a hypersonic airplane configuration at Mach numbers of 1.41, 2.01, and 6.86.
- OCLC:
- 761192031
The Penn Libraries is committed to describing library materials using current, accurate, and responsible language. If you discover outdated or inaccurate language, please fill out this feedback form to report it and suggest alternative language.