Download Free Large Scale Wind Tunnel Tests Of Airplane Model With Unswept Aspect Ratio 10 Wing 2 Propellers And Blowing Flaps With List Of References Book in PDF and EPUB Free Download. You can read online Large Scale Wind Tunnel Tests Of Airplane Model With Unswept Aspect Ratio 10 Wing 2 Propellers And Blowing Flaps With List Of References and write the review.

Tests were made of a large-scale tilt-wing deflected-slipstream VTOL airplane with blowingtype BLC trailing-edge flaps. The model was tested with flap deflections of 0 degrees without BLC, 50 degrees with and without BLC, and 80 degrees with BLC for wing-tilt angles of 0, 30, and 50 degrees. 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. (Author).
February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index.
Tests were conducted to determine the wing stall, performance, and longitudinal stability and control characteristics of a large model of a V/STOL tilt-wing transport aircraft. The scope of the tests was limited primarily to the low-speed transitional regime.