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- W272644832 abstract "Report presenting an investigation of the F9F-4 airplane to evaluate a high-energy blowing boundary-layer-system in flight in order to improve the maximum lift characteristics of airplane wings. A high-energy blowing-boundary-layer control system was installed by the Grumman Aircraft Engineering Corporation. A series of test flights were made to measure the lift and drag variations with changes in angle of attack for the flap and gear both up and down and for blowing on and off." @default.
- W272644832 created "2016-06-24" @default.
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- W272644832 date "1956-02-14" @default.
- W272644832 modified "2023-09-24" @default.
- W272644832 title "A Flight Evaluation of a Wing-shroud-blowing Boundary-layer Control System Applied to the Flaps of an F9F-4 Airplane" @default.
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