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.
Flutter of a Low-aspect-ratio Rectangular Wing
Flutter and Divergence of Rectangular Wings of Very Low Aspect Ratio
Flutter Analysis of Low Aspect Ratio Straight Wings in the Transonic Region
Flutter of Low Aspect-ratio Wings: Calculation of pressure distribution for oscillating wings of arbitrary planform in subsonic flow by the kernel-function methods, by Pao-Tan Hsu
Author: Massachusetts Institute of Technology
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 60
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 60
Book Description
Flutter Investigation of Two Thin, Low-aspect-ratio, Swept, Solid, Metal Wings in the Transonic Range by Use of Free-falling Body
Author: W. T. Lauten
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 18
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 18
Book Description
Flutter Analyses of Two Low-aspect-ratio Wings
Author: Herbert M. Voss
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 59
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 59
Book Description
Technical Note - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 966
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 966
Book Description
Some Low-speed Flutter Characteristics of Simple Low-aspect-ratio Delta Wing Models
Author: Robert V. Doggett (Jr)
Publisher:
ISBN:
Category :
Languages : en
Pages : 11
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 11
Book Description