Exhaust environment measurements of a turbofan engine equipped with an afterburner and 2D nozzle
By: L.O. Brase.
Contributors: McDonnell Aircraft Company.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.; Lewis Research Center.
Series: NASA contractor report -- 4289.; NASA contractor report -- NASA CR-4289.
Publisher: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division; For sale by the National Technical Information Service
Published: 1990
Place of publication: [Washington, D.C.]; Springfield, Va
Language: eng
Format: Microform
Number of pages: 55
Subjects: Airplanes -- Turbofan engines -- Noise -- Measurement.; Afterburning.; Divergent nozzles.; Exhaust gases.; Exhuast nozzles.; Jet aircraft noise.; Noise measurement.; Pressure measurement.; Structural vibration.; Turbofan engines.
Notes: Shipping list no.: 1990-0882-M.

Distributed to depository libraries in microfiche.

"May 1990."

Prepared at McDonnell Aircraft Company for Lewis Research Center.

Bibliography: p. 55.

Also available via Internet from the NTRS web site. Address as of 4/25/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900012444%5F1990012444.pdf; current access is available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration,] 1990. 1 microfiche.