Experimental aerodynamic characteristics for slender bodies with thin wings and tail at angles of attack from 0 ̊to 58 ̊and Mach from 0.6 to 2.0
- Image
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- Created Date
- 1976
- Description
Cover title.
Includes bibliographical references (p. 9).
- Creator
Jorgensen, Leland H
- Partner
- HathiTrust
- Contributing Institution
- University of Illinois
- Publisher
- Washington : U.S. National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service
- Subjects
- Mach number
Aerodynamics - Type
- text
- Format
- Language materialElectronic resource
- Language
- English
- Rights
- Public domain. Learn more at http://www.hathitrust.org/access_use
- Chicago citation style
- Jorgensen, Leland H. Experimental aerodynamic characteristics for slender bodies with thin wings and tail at angles of attack from 0 ̊to 58 ̊and Mach from 0.6 to 2.0. 1976. Retrieved from the Digital Public Library of America, http://catalog.hathitrust.org/Record/011427467. (Accessed April 18, 2024.)
- APA citation style
- Jorgensen, Leland H, (1976) Experimental aerodynamic characteristics for slender bodies with thin wings and tail at angles of attack from 0 ̊to 58 ̊and Mach from 0.6 to 2.0. Retrieved from the Digital Public Library of America, http://catalog.hathitrust.org/Record/011427467
- MLA citation style
- Jorgensen, Leland H. Retrieved from the Digital Public Library of America <http://catalog.hathitrust.org/Record/011427467>.