An investigation of two variations of the gas generator method to calculate the thrust of the afterburning turbofan engines installed in an F-111A airplane /
Frank W. Burcham, Jr.

Description

Main Author: Burcham, Frank W.
Language(s): English
Published: Washington, D.C.: National Aeronautics and Space Administration: 1971.
Subjects: F-111 (Jet fighter plane)
Airplanes > Airplanes / Turbofan engines > Airplanes / Turbofan engines / Afterburners.
Airplanes > Airplanes / Motors > Airplanes / Motors / Thrust > Airplanes / Motors / Thrust / Measurement.
Physical Description: 29 p. ill.; 27 cm.
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Item Link	Original Source
Full view	University of Illinois at Urbana-Champaign