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Investigation of ground effects on large and small scale models of a three fan V/STOL aircraft configuration (1979)

Schuster, E. P. ; Carter, T. D. ; Esker, D. W.

In: CASI

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Publication Date: 2019-06-27

Description: Induced lift of a subsonic, three fan, lift/cruise, V/STOL aircraft configuration was investigated using scale modes of a multimission aircraft whose design incorporates a nose mounted lift fan and two lift/cruise units located over the wing. Configuration effects were assessed for lift improvement devices, lift/cruise nozzle rails, nozzle perimeter plates, and alternate nose fan exit hubs. Tests were conducted at four model heights (H/D = 0.95, 1.53, 3.06 and 6.45, where D is the average nozzle exit diameter equal to 0.997 m.) Results are presented and discussed.

Keywords: AERODYNAMICS

Type: NASA-CR-152240 , MDC-A5702

Format: application/pdf

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