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NASA Technical Note [NASA TN D-6297]: An investigation of two variations of the gas generator method to calculate the thrust of the afterburning turbofan engines installed in an F111A airplane

By: Washington. National Aeronautics and Space Administration (NASA).
Contributor(s): Burcham, Frank W.
Material type: materialTypeLabelBookSeries: National Aeronautics and Space Administration ; NASA Technical Note. Publisher: Washington NASA 1971Description: 29p.Subject(s): Aircraft | Propulsion systems | Thurst measurement
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