![Large Scale Wind-tunnel Tests of Airplane Model with Unswept, Aspect-ratio-10 Wing, 2 Propellers, and Blowing Flaps [with List of References] PDF](https://books.google.com/books/content/images/frontcover/vhRgswEACAAJ?fife=w80-h100)
Author: Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 47
Book Description
Large Scale Wind-tunnel Tests of Airplane Model with Unswept, Aspect-ratio-10 Wing, 2 Propellers, and Blowing Flaps [with List of References]
Author: Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 47
Book Description
Large-scale Wind-tunnel Tests of an Airplane Model with an Unswept, Tilt Wing of Aspect Ration 5.5, and with Four Propellers and Blowing Flaps
Author: James A. WeibergPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 38
Book Description
Large-scale Wind-tunnel Tests of an Airplane Model with an Unswept, Aspect-ratio-10 Wing, Two Propellers, and Blowing Flaps
Author: Roy N. GriffinPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 47
Book Description
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 Flaps
Author: James A. WeibergPublisher:
ISBN:
Category :
Languages : en
Pages : 31
Book Description
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 Flap
Author: NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON D C.Publisher:
ISBN:
Category :
Languages : en
Pages : 1
Book Description
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).
Large-scale Wind-tunnel Tests of an Airplane Model with an Unswept Tilt Wing of Aspect Ratio 5.5, and with Various Stall Control Devices
Author: James A. WeibergPublisher:
ISBN:
Category : Buffeting (Aerodynamics)
Languages : en
Pages : 54
Book Description
Large-scale Wind-tunnel Tests of an Airplane Model with an Unswept, Tilt Wing of Aspect Ration 5.5, and with Four Propellers and Blowing Flaps
Author: James A. WeibergPublisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
Large-scale Wind-tunnel Tests of an Airplane Model with Two Propellers and Rotaing Cylinder Flaps
Author: James A. WeibergPublisher:
ISBN:
Category : Flaps (Airplanes)
Languages : en
Pages : 60
Book Description
Monthly Catalog of United States Government Publications
Author: United States. Superintendent of DocumentsPublisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1714
Book Description
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.
Full-scale Wind-tunnel Tests of a Low-aspect-ratio, Straight-wing Airplane with Blowing Boundary-layer Control on Leading- and Trailing-edge Flaps
Author: Mark W. KellyPublisher:
ISBN:
Category : Trailing edge flaps
Languages : en
Pages : 32
Book Description
