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- W774319991 abstract "Key results from low speed wind tunnel testing of the F-15 STOL and Maneuver Technology Demonstrator (SMDT) with thrust reversers are presented. Longitudinally, the largest induced increments in the stability and control occur at landing gear height. These generally reflect an induced lift loss and a nose-up pitching moment, and vary with sideslip. Directional stability is reduced at landing gear height with full reverse thrust. Nonlinearities in the horizontal tail effectiveness are found in free air and at landing gear height." @default.
- W774319991 created "2016-06-24" @default.
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- W774319991 date "1988-02-01" @default.
- W774319991 modified "2023-09-27" @default.
- W774319991 title "F-15 SMTD low speed jet effects wind tunnel test results" @default.
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