Combustion stability of single swirl-can combustor modules using ASTM-A1 liquid fuel
- Image
- View Full Item
- Created Date
- 1969]
- Description
Prepared at Lewis Research Center.
"October 1969."
Cover title.
Includes bibliographical references (p. 27).
Combustion stability of single swirl-can combustor modules using ASTM-A1 liquid fuel.
- Creator
Niedzwiecki, Richard W
- 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
- Airplanes--Motors--Carburetors--Testing
Airplanes--Turbojet engines--Combustion--Equipment and supplies--Testing
Aircraft gas-turbines--Combustion chambers--Testing - Type
- text
- Format
- Language materialElectronic resource
- Language
- English
- Rights
- Public domain. Learn more at http://www.hathitrust.org/access_use
- Chicago citation style
- Niedzwiecki, Richard W. Combustion stability of single swirl-can combustor modules using ASTM-A1 liquid fuel. 1969]. Retrieved from the Digital Public Library of America, http://catalog.hathitrust.org/Record/011444173. (Accessed March 28, 2024.)
- APA citation style
- Niedzwiecki, Richard W, (1969]) Combustion stability of single swirl-can combustor modules using ASTM-A1 liquid fuel. Retrieved from the Digital Public Library of America, http://catalog.hathitrust.org/Record/011444173
- MLA citation style
- Niedzwiecki, Richard W. Retrieved from the Digital Public Library of America <http://catalog.hathitrust.org/Record/011444173>.