Flutter Design of Stiffened-skin Panels for Hypersonic Aircraft

Flutter Design of Stiffened-skin Panels for Hypersonic Aircraft PDF Author: Herman L. Bohon
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 36

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Book Description
Design factors for flutter control of stiffened exterior skin panels for hypersonic aircraft.

Flutter Design of Stiffened-skin Panels for Hypersonic Aircraft

Flutter Design of Stiffened-skin Panels for Hypersonic Aircraft PDF Author: Herman L. Bohon
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 36

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Book Description
Design factors for flutter control of stiffened exterior skin panels for hypersonic aircraft.

Flutter Design of Stiffened-skin Panels for Hypersonic Aircraft

Flutter Design of Stiffened-skin Panels for Hypersonic Aircraft PDF Author: Herman L. Bohon
Publisher:
ISBN:
Category : Corrugation-stiffened panels
Languages : en
Pages : 26

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Conference on Hypersonic Aircraft Technology

Conference on Hypersonic Aircraft Technology PDF Author:
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 590

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NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 446

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Natural Vibration and Flutter of Elastically Supported Corrugation-stiffened Panels

Natural Vibration and Flutter of Elastically Supported Corrugation-stiffened Panels PDF Author: Walter L. Heard
Publisher:
ISBN:
Category : Flutter (Aerodynamics)
Languages : en
Pages : 44

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Book Description
The natural vibration and flutter characteristics of two corrugation-stiffened panels were studied experimentally and theoretically to determine the effects of finite deflectional, rotational, and torsional stiffnesses of the boundary supports. Flutter tests were conducted at a Mach number of 3. The experimental data are compared with results from a flutter theory for orthotropic panels which includes the effects of finite support stiffnesses as well as uniform in-plane loading of the panel. The investigation indicates that finite deflectional, rotational, and torsional stiffnesses of the boundary supports must be accounted for in the theory in order to match experimental natural frequencies of the test panels. However, it is concluded that structural damping (neglected in the theory) strongly influenced the flutter behavior of the test panels. Furthermore, the theory shows that the addition of torsional stiffening at the supports is a definite asset for increasing flutter dynamic pressure and may be extremely important in the design of panels for application at hypersonic speeds where thermal expansion may be desired.

Monthly Catalogue, United States Public Documents

Monthly Catalogue, United States Public Documents PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1250

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Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1464

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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1460

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Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.

Design Procedures for Flutter-free Surface Panels

Design Procedures for Flutter-free Surface Panels PDF Author: Robert M. Laurenson
Publisher:
ISBN:
Category : Airframes
Languages : en
Pages : 132

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U.S. Government Research & Development Reports

U.S. Government Research & Development Reports PDF Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 212

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