Supersonic Aeroelastic Effects on Static Stability and Control: Aeroelastic interaction, by V. W. Donato PDF Download
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Author: Bell Aircraft Corporation
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 374
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Book Description
Author: Bell Aircraft Corporation
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 374
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Book Description
Author: Ivan Rattinger
Publisher:
ISBN:
Category :
Languages : en
Pages : 325
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Book Description
Author: Ivan Rattinger
Publisher:
ISBN:
Category :
Languages : en
Pages :
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Book Description
Author: Floyd V. Bennett
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 48
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Book Description
Wind tunnel tests showing the effects of static aeroelasticity for a thin 45° delta wing in supersonic flow are presented and compared with theory in the Mach number range 1.30 t o 4.00. Calculated deformations, normal-force coefficients, and pitching-moment coefficients based on a linearized potential theory for subsonic leading edges at a Mach number of 1.30 and a linearized potential theory for supersonic leading edges at Mach numbers of 1.64, 3.00, and 4.00 are shown to compare favorably with the wind-tunnel results.
Author: James R. Batt
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 190
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Author: James R. Batt
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 392
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Book Description
Author: M. Leroy Spearman
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 22
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Book Description
Author: Jesse L. Mitchell
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 32
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Book Description
Author: Courtland D. Perkins
Publisher: Elsevier
ISBN: 1483222330
Category : Technology & Engineering
Languages : en
Pages : 520
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Book Description
Flight Testing, Volume II: Stability and Control focuses on the development of adequate flight test techniques for the appraisal of stability and control characteristics and flying qualities of airplanes. This book discusses the flying quality requirements, longitudinal motions, and flight determination of stick-fixed neutral points. The determination of aerodynamic parameters from steady maneuvering, desirable control characteristics in steady flight, and various forms of lateral control surfaces are also elaborated. This publication likewise covers the measurement of maximum lift coefficient, emergency anti-spin devices, and concept of the altitude-Mach number flight envelope. This volume is recommended for design, development or research engineers, test pilots, and instrumentation personnel interested in airplane stability and control.
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 442
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