Flow analysis and design optimization methods for nozzle afterbody of a hypersonic vehicle
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- Created Date
- 1992
- Description
Prepared at the Mechanical Engineering and Mechanics Dept., Old Dominion University, for Langley Research Center under Grants NAG1-811 and NAG1-1188.
Includes bibliographical references (p. 24-26).
- Creator
Baysal, Oktay
- Partner
- HathiTrust
- Contributing Institution
- University of Illinois
- Publisher
- Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Subjects
- Aircraft exhaust emissions
Airplanes--Ramjet engines
Jet nozzles--Design and construction
Aerodynamics, Hypersonic - Type
- text
- Format
- Language materialElectronic resource
- Language
- English
- Rights
- Public domain. Learn more at http://www.hathitrust.org/access_use
- Chicago citation style
- Baysal, Oktay. Flow analysis and design optimization methods for nozzle afterbody of a hypersonic vehicle. 1992. Retrieved from the Digital Public Library of America, http://catalog.hathitrust.org/Record/011431856. (Accessed March 28, 2024.)
- APA citation style
- Baysal, Oktay, (1992) Flow analysis and design optimization methods for nozzle afterbody of a hypersonic vehicle. Retrieved from the Digital Public Library of America, http://catalog.hathitrust.org/Record/011431856
- MLA citation style
- Baysal, Oktay. Retrieved from the Digital Public Library of America <http://catalog.hathitrust.org/Record/011431856>.