Measurement effects on the calculation of in-flight thrust for an F404 turbofan engine
By: Timothy R. Conners.
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.
Series: NASA technical memorandum -- 4140.
Publisher: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division; For sale by the National Technical Information Service]
Published: 1989
Place of publication: [Washington, D.C.]; [Springfield, VA
Language: eng
Format: Microform
Number of pages: 21
Subjects: Airplanes -- Motors -- Thrust -- Measurement.; Airplanes -- Turbofan engines -- Testing.; Afterburning.; In-flight monitoring.; Thrust measurement.; Turbofan engines.
Notes: Shipping list no.: 90-0398-M.

"Performing organization report no.: H-1556"--Technical rept. documentation p.

Includes bibliographical references (p. 8).

Also available via Internet from the NASA Technical Report Server web site. Address as of 7/28/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900002425%5F1990002425.pdf; current access available via PURL.

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

RTOP 533-02-51.