Author: Robert William Fralich
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 652
Book Description
A flutter analysis, employing slender-body aerodynamic theory and thin-plate theory, is made for rectangular wings of very low aspect ratio with a constant thickness. The spanwise variation of wing deflection is assumed to be given by a parabola, and the chordwise variation is allowed complete freedom. The results show the vsriation of flutter speed and male shape with aspect ratio. Comparisons are made with additional resuits obtained by approximating the chordwise deflection shape by use of parabolic or cubic curves. The analysis shows that the cubic approximation gives good resuits for a ratio of chord to semispan less than 3.
Flutter Analysis of Rectangular Wings of Very Low Aspect Ratio
Author: Robert William Fralich
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 652
Book Description
A flutter analysis, employing slender-body aerodynamic theory and thin-plate theory, is made for rectangular wings of very low aspect ratio with a constant thickness. The spanwise variation of wing deflection is assumed to be given by a parabola, and the chordwise variation is allowed complete freedom. The results show the vsriation of flutter speed and male shape with aspect ratio. Comparisons are made with additional resuits obtained by approximating the chordwise deflection shape by use of parabolic or cubic curves. The analysis shows that the cubic approximation gives good resuits for a ratio of chord to semispan less than 3.
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 652
Book Description
A flutter analysis, employing slender-body aerodynamic theory and thin-plate theory, is made for rectangular wings of very low aspect ratio with a constant thickness. The spanwise variation of wing deflection is assumed to be given by a parabola, and the chordwise variation is allowed complete freedom. The results show the vsriation of flutter speed and male shape with aspect ratio. Comparisons are made with additional resuits obtained by approximating the chordwise deflection shape by use of parabolic or cubic curves. The analysis shows that the cubic approximation gives good resuits for a ratio of chord to semispan less than 3.
NACA Conference on Aircraft Loads, Structures, and Flutter
Comparative Evaluation of Methods for Predicting Flutter and Divergence of Unswept Wings of Finite Span
Author: Edward Carson Yates
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 62
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 62
Book Description
NACA Research Memorandum
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 610
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 610
Book Description
NASA Technical Note
Principles of Aeroelasticity
Author: Raymond L. Bisplinghoff
Publisher: Courier Corporation
ISBN: 0486783162
Category : Technology & Engineering
Languages : en
Pages : 545
Book Description
Geared toward professional engineers, this volume will be helpful for students, too. Topics include methods of constructing static and dynamic equations, heated elastic solids, forms of aerodynamic operators, structural operators, and more. 1962 edition.
Publisher: Courier Corporation
ISBN: 0486783162
Category : Technology & Engineering
Languages : en
Pages : 545
Book Description
Geared toward professional engineers, this volume will be helpful for students, too. Topics include methods of constructing static and dynamic equations, heated elastic solids, forms of aerodynamic operators, structural operators, and more. 1962 edition.
A Selected Listing of NASA Scientific and Technical Reports for ...
Index of N A S A Technical Publications
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category :
Languages : en
Pages : 498
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 498
Book Description
Experimental and Calculated Results of a Flutter Investigation of Some Very Low Aspect-ratio Flat-plate Surfaces at Mach Numbers from 0.62 to 3.00
Author: Perry W. Hanson
Publisher:
ISBN:
Category : Flat plates
Languages : en
Pages : 30
Book Description
Publisher:
ISBN:
Category : Flat plates
Languages : en
Pages : 30
Book Description
Monthly Catalogue, United States Public Documents
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1690
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1690
Book Description