Effect of injection element radial distribution and chamber geometry on acoustic-mode instability in a hydrogen oxygen rocket
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- Created Date
- [1969]
- Description
Prepared at Lewis Research Center.
"August 1969"--Cover.
Includes bibliographical references (p. 30).
Injector radial distribution and thrust chamber geometry effect on acoustic mode instability in hydrogen oxygen engines.
- Creator
Wanhainen, John P
- Partner
- HathiTrust
- Contributing Institution
- University of Illinois
- Publisher
- Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information
- Subjects
- Liquid propellant rocket engines
Liquid propellant rockets--Fuel systems
Rocket engines--Combustion - Type
- text
- Format
- Language materialElectronic resource
- Language
- English
- Rights
- Public domain. Learn more at http://www.hathitrust.org/access_use
- Chicago citation style
- Wanhainen, John P. Effect of injection element radial distribution and chamber geometry on acoustic-mode instability in a hydrogen oxygen rocket. [1969]. Retrieved from the Digital Public Library of America, http://catalog.hathitrust.org/Record/011444642. (Accessed April 16, 2024.)
- APA citation style
- Wanhainen, John P, ([1969]) Effect of injection element radial distribution and chamber geometry on acoustic-mode instability in a hydrogen oxygen rocket. Retrieved from the Digital Public Library of America, http://catalog.hathitrust.org/Record/011444642
- MLA citation style
- Wanhainen, John P. Retrieved from the Digital Public Library of America <http://catalog.hathitrust.org/Record/011444642>.