Unsteady Surface Pressure Distributions on a Delta Wing Undergoing Large Amplitude Pitching Motions PDF Download
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Author: S. A. Thompson
Publisher:
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Category :
Languages : en
Pages :
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Author: S. A. Thompson
Publisher:
ISBN:
Category :
Languages : en
Pages :
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Author: Scott Andrew Thompson
Publisher:
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Category :
Languages : en
Pages : 452
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Author: Scott A. Thompson
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Category :
Languages : en
Pages : 314
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Author: Scott Andrew Thompson
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ISBN:
Category :
Languages : en
Pages : 0
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Author: Yahia A. Abdelhamid
Publisher:
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Category : Airplanes
Languages : en
Pages : 430
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Author: Mohammad-Ameen M. Jarrah
Publisher:
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Category : Aerodynamics
Languages : en
Pages : 352
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Category : Aeronautics
Languages : en
Pages : 530
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Author: Andrew S. Arena
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Category :
Languages : en
Pages :
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Author: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Fluid Dynamics Panel. Special Course
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 154
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Book Description
"This report consists of lecture notes of an AGARD Fluid Dynamics Panel Special Course. These notes provide the latest information on the development and use of dynamic experiments in wind tunnels from several of the NATO nations. They address current oscillatory and rotary test techniques, experimental results for typical configurations, and the use of these data for flight mechanics applications. Subject included are: dynamic lift, wing rock, fluid dynamics of rotary flows, mathematical modelling, non-linear data representation, vortex manipulation for control enhancement, and correlations of predictions based on rotary and oscillatory wind-tunnel and flight-test results. The complete course notes are contained in two volumes. The main part of the notes is contained in AGARD Advisory Report 265 (ADA235179). The present volume includes papers on: Unsteady aerodynamics of slender wings; Dynamic stall effects and applications to high performance aircraft; Oscillatory test techniques; Large amplitude oscillations; Oscillatory data for typical configurations; and Forebody vortex control."--Stinet.
Author: Michael J. Hemsch
Publisher: AIAA (American Institute of Aeronautics & Astronautics)
ISBN:
Category : Science
Languages : en
Pages : 774
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Book Description
This two-volume set includes discussions of the physics of the fluid mechanics phenomena associated with tactical missile flight and the full range of prediction methods required to analyze current and future missiles. It's a valuable resource for missile aerodynamicists, designers, and researchers.
