Thrust performance of isolated 36-chute suppressor plug nozzles with and without ejectors at Mach numbers from 0 to 0.45
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- Created Date
- 1975
- Description
Prepared at Lewis Research Center.
Cover title.
Includes bibliographical references (p. 12-14).
- Creator
Harrington, Douglas E
- Partner
- HathiTrust
- Contributing Institution
- University of Illinois
- Publisher
- Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service]
- Subjects
- Jet planes--Noise
Airplanes--Turbojet engines--Mufflers
Airplanes--Motors--Thrust
Jet nozzles--Testing - Type
- text
- Format
- Language materialElectronic resource
- Language
- English
- Rights
- Public domain. Learn more at http://www.hathitrust.org/access_use
- Chicago citation style
- Harrington, Douglas E. Thrust performance of isolated 36-chute suppressor plug nozzles with and without ejectors at Mach numbers from 0 to 0.45. 1975. Retrieved from the Digital Public Library of America, http://catalog.hathitrust.org/Record/011427266. (Accessed March 28, 2024.)
- APA citation style
- Harrington, Douglas E, (1975) Thrust performance of isolated 36-chute suppressor plug nozzles with and without ejectors at Mach numbers from 0 to 0.45. Retrieved from the Digital Public Library of America, http://catalog.hathitrust.org/Record/011427266
- MLA citation style
- Harrington, Douglas E. Retrieved from the Digital Public Library of America <http://catalog.hathitrust.org/Record/011427266>.