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Static stability and control characteristics of an airplane model with tail surfaces outboard of the wing tips at a mach number of 2.01 / by Cornelius Driver and M. Leroy Spearman.
Connect to full text Available online
View online- Format:
- Book
- Government document
- Author/Creator:
- Driver, Cornelius, author.
- Spearman, M. Leroy, author.
- Series:
- NASA technical memorandum ; X-47.
- NASA/TM ; X-47
- Language:
- English
- Subjects (All):
- Stability of airplanes.
- Airplanes--Tail surfaces.
- Airplanes.
- Aerodynamics, Supersonic.
- Physical Description:
- 1 online resource (28 pages) : illustrations
- Place of Publication:
- Washington : National Aeronautics and Space Administration, September 1959.
- System Details:
- Master and use copy. Digital master created according to Benchmark for Faithful Digital Reproductions of Monographs and Serials, Version 1. Digital Library Federation, December 2002. http://purl.oclc.org/DLF/benchrepro0212
- Notes:
- Cover title.
- "September 1959."
- In scope of the U.S. Government Publishing Office Cataloging and Indexing Program (C&I) and Federal Depository Library Program (FDLP).
- Includes bibliographical references (page 8).
- Electronic reproduction. [Place of publication not identified]: HathiTrust Digital Library. 2024.
- Description based on online resource; title from PDF title page (NASA, viewed Nov. 25, 2024).
- OCLC:
- 1419919977
- Access Restriction:
- Use copy Restrictions unspecified
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