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Large Scale Wind Tunnel Investigation Of An Airplane Model With A Tilt Wing Of Aspect Ratio 84 And Four Propellers In The Presence Of A Ground Plane
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Book Synopsis Large-scale Wind-tunnel Investigation of an Airplane Model with a Tilt Wing of Aspect Ratio 8.4, and Four Propellers, in the Presence of a Ground Plane by : Stanley O. Dickinson
Download or read book Large-scale Wind-tunnel Investigation of an Airplane Model with a Tilt Wing of Aspect Ratio 8.4, and Four Propellers, in the Presence of a Ground Plane written by Stanley O. Dickinson and published by . This book was released on 1968 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Large-scale Wind-tunnel Investigation of an Airplane Model with a Tilt Wing of Aspect Ratio 8.4, and Four Propellers, in the Presence of a Ground Plane by : Stanley O. Dickinson
Download or read book Large-scale Wind-tunnel Investigation of an Airplane Model with a Tilt Wing of Aspect Ratio 8.4, and Four Propellers, in the Presence of a Ground Plane written by Stanley O. Dickinson and published by . This book was released on 1968 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Large Wind-tunnel Investigation of an Airplane Model with a Tilt Wing of Aspect Ratio 8.4, and Four Propellers, in the Presence of a Ground Plane by : Stanley O. Dickinson
Download or read book Large Wind-tunnel Investigation of an Airplane Model with a Tilt Wing of Aspect Ratio 8.4, and Four Propellers, in the Presence of a Ground Plane written by Stanley O. Dickinson and published by . This book was released on 1968 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis 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 by : NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON D C.
Download or read book 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 written by NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON D C. and published by . This book was released on 1961 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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).
Book Synopsis Summary of a Flight-test Evaluation of the CL-84 Tilt-wing V/STOL Aircraft by : Robert A. Champine
Download or read book Summary of a Flight-test Evaluation of the CL-84 Tilt-wing V/STOL Aircraft written by Robert A. Champine and published by . This book was released on 1970 with total page 94 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis 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 by : James A. Weiberg
Download or read book 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 written by James A. Weiberg and published by . This book was released on 1961 with total page 31 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Large-scale Wind-tunnel Tests at Low Speed of a Delta Winged Supersonic Transport Model in the Presence of the Ground by :
Download or read book Large-scale Wind-tunnel Tests at Low Speed of a Delta Winged Supersonic Transport Model in the Presence of the Ground written by and published by . This book was released on 1962 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Large-scale Wind-tunnel Investigation of an Airplane Model with a Tilt Wing by : Stanley O. Dickinson
Download or read book Large-scale Wind-tunnel Investigation of an Airplane Model with a Tilt Wing written by Stanley O. Dickinson and published by . This book was released on 1968 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis 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 by : James A. Weiberg
Download or read book 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 written by James A. Weiberg and published by . This book was released on 1961 with total page 33 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Large-scale Wind-tunnel Tests of an Airplane Model with an Unswept, Aspect-ratio-10 Wing, Two Propellers, and Blowing Flaps by : Roy N. Griffin
Download or read book Large-scale Wind-tunnel Tests of an Airplane Model with an Unswept, Aspect-ratio-10 Wing, Two Propellers, and Blowing Flaps written by Roy N. Griffin and published by . This book was released on 1958 with total page 47 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis 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 by : James A. Weiberg
Download or read book 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 written by James A. Weiberg and published by . This book was released on 1964 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Large Scale Wind-tunnel Tests of Airplane Model with Unswept, Aspect-ratio-10 Wing, 2 Propellers, and Blowing Flaps [with List of References] by :
Download or read book Large Scale Wind-tunnel Tests of Airplane Model with Unswept, Aspect-ratio-10 Wing, 2 Propellers, and Blowing Flaps [with List of References] written by and published by . This book was released on 1958 with total page 47 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Large-scale Wind-tunnel Tests of a Deflected Slipstream STOL Model with Wings of Various Aspect Ratios by : V. Robert Page
Download or read book Large-scale Wind-tunnel Tests of a Deflected Slipstream STOL Model with Wings of Various Aspect Ratios written by V. Robert Page and published by . This book was released on 1968 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Buffeting Measurements on Two Wing End-plate Airplane Model Configurations by : William B. Igoe
Download or read book Wind-tunnel Buffeting Measurements on Two Wing End-plate Airplane Model Configurations written by William B. Igoe and published by . This book was released on 1967 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Large-scale Wind-tunnel Tests of an Airplane Model with a 45 Degree Sweptback Wing of Aspect Ratio 2.8 with Area Suction Applied to Trailing-edge Flaps and with Several Wing Leading-edge Modifications by : David G. Koenig
Download or read book Large-scale Wind-tunnel Tests of an Airplane Model with a 45 Degree Sweptback Wing of Aspect Ratio 2.8 with Area Suction Applied to Trailing-edge Flaps and with Several Wing Leading-edge Modifications written by David G. Koenig and published by . This book was released on 1956 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation of an airplane model was conducted to determine the effect of area-suction trailing-edge flaps and several leading-edge modifications on the aerodynamic characteristics of a 45 degree sweptback wing. The wing had an aspect ratio of 2.8 and a taper ratio of 0.17. The wing was tested with a small-span constant-chord flap and, to a lesser extent, with a larger span constant-percent wing-chord flap. Area suction was applied to both flaps. Leading-edge flaps are modified leading-edge contours were tested in an effort to produce adequate leading-edge stall control. A chord extension and a fence were also tested. Part of the testing was done with a horizontal tail installed above the extended wing-chord plane. The tests were made at a Reynolds number of 10,000,000.
Book Synopsis Wind Tunnel Investigation of a Large-scale Upper Surface Blown-flap Model Having Four Engines by :
Download or read book Wind Tunnel Investigation of a Large-scale Upper Surface Blown-flap Model Having Four Engines written by and published by . This book was released on 1975 with total page 86 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind Tunnel Investigation of an Aspect Ratio 10 Tandem Wing Aircraft Configuration in Ground Effect. Part Ii. Lateral Characterization by : Lynn A. Trobaugh
Download or read book Wind Tunnel Investigation of an Aspect Ratio 10 Tandem Wing Aircraft Configuration in Ground Effect. Part Ii. Lateral Characterization written by Lynn A. Trobaugh and published by . This book was released on 1967 with total page 53 pages. Available in PDF, EPUB and Kindle. Book excerpt: Subsonic wind tunnel test results obtained to determine the lateral aerodynamic characteristics of a tandem wing aircraft model in and out of ground effect are given. Test variables included model height above a ground board, model angle of attack, model angle of sideslip, and center-of-gravity location. Ground effect causes large sideslip-induced rolling moments (dihedral effect) on the model, which can be moderated by altering the size of the vertical tail. It is also possible that the large dihedral effect would be moderated by the roll stiffness term. However, roll stiffness data were not obtained for this model. (Author).
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