Large-scale Wind-tunnel Tests of a Circulation Plan-form Aircraft with a Peripheral Jet for Lift, Thrust, and Control PDF Download
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Author: Richard K. Grief
Publisher:
ISBN:
Category : Jet planes
Languages : en
Pages : 112
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Book Description
Author: Richard K. Grief
Publisher:
ISBN:
Category : Jet planes
Languages : en
Pages : 112
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Book Description
Author: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development
Publisher:
ISBN:
Category : Short take-off and landing aircraft
Languages : en
Pages : 344
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Book Description
Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 258
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Book Description
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 262
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Book Description
Author:
Publisher:
ISBN:
Category : Ground-effect machines
Languages : en
Pages : 388
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 262
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Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 254
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Book Description
Author:
Publisher:
ISBN:
Category : Engineering
Languages : en
Pages : 1204
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Book Description
Author: Barnes Warnock McCormick
Publisher: Courier Corporation
ISBN: 9780486404608
Category : Technology & Engineering
Languages : en
Pages : 356
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Book Description
An extremely practical overview of V/STOL (vertical/short takeoff and landing) aerodynamics, this volume offers a presentation of general theoretical and applied aerodynamic principles, covering propeller and helicopter rotor theory for both the static and forward flight cases. Both a text for students and a reference for professionals, the book can be used for advanced undergraduate or graduate courses. Numerous detailed figures, plus exercises. 1967 edition. Preface. Appendix. Index.
Author: Paul T. Soderman
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 108
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Book Description
The aerodynamic characteristics of a full scale executive type jet transport aircraft with a T-tail were investigated in a 40 x 80 ft (12.2 by 24.4 meter) wind tunnel (subsonic). Static, longitudinal, and lateral stability, and control characteristics were determined at angles of attack from -2 deg to 42 deg. The aircraft wing had 13 deg of sweep and an aspect ratio of 5.02. The aircraft was tested power off with various wing leading- and trailing-edge high lift devices. The basic configuration was tested with and without such components as engine nacelles, wing tip tanks, and empannage. Hinge-moment data were obtained and downwash angles in the horizontal-tail plane location were calculated. The data were obtained at Reynolds numbers of 4.1 million and 8.7 million based on mean aerodynamic chord. The model had static longitudinal stability through initial stall. Severe tail buffet occurred near the angle of attack for maximum lift. Above initial stall the aircraft had pronounced pitch-up, characteristic of T-tail configurations. A stable trim point was possible at angles of attack between 30 deg and 40 deg (depending on c.g. location and flap setting). Hinge-moment data showed no regions with adverse effects on stick force. Comparisons of wind-tunnel data and flight-test are presented.
