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Large-Scale Wind-Tunnel Tests of an Airplane Model with an Unswept, Tilt Wing of Aspect Ratio 5.5, and with Four Propellers and Blowing FlapsTests were made of a large-scale tilt-wing deflected-slipstream VTOL airplane with blowing-type BLC trailing-edge flaps. The model was tested with flap deflections of 0 deg. without BLC, 50 deg. with and without BLC, and 80 deg. with BLC for wing-tilt angles of 0, 30, and 50 deg. Included are results of tests of the model equipped with a leading-edge flap and the results of tests of the model in the presence of a ground plane.
Document ID
19980227077
Acquisition Source
Headquarters
Document Type
Other - NASA Technical Note (TN)
Authors
Weiberg, James A. (NASA Ames Research Center Moffett Field, CA United States)
Holzhauser, Curt A. (NASA Ames Research Center Moffett Field, CA United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1961
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-1034
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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