Author: Joseph A. Drischler
Publisher:
ISBN:
Category : Air flow
Languages : en
Pages : 26
Book Description
The unsteady-lift functions for a wing undergoing a sudden change in sinking speed have been presented for delta wings having aspect ratios of 0, 2, and 4 and for rectangular and elliptical wings having aspect ratios of 0, 3, and 6. For the elliptical and rectangular wings the spanwise lift distributions were also presented. These functions were calculated from the lift coefficients associated with a wing oscillating harmonically in pure translational motion, as obtained from several sources.
Approximate Indicial Lift Functions for Several Wings of Finite Span in Incompressible Flow as Obtained from Oscillatory Lift Coefficients
Author: Joseph A. Drischler
Publisher:
ISBN:
Category : Air flow
Languages : en
Pages : 26
Book Description
The unsteady-lift functions for a wing undergoing a sudden change in sinking speed have been presented for delta wings having aspect ratios of 0, 2, and 4 and for rectangular and elliptical wings having aspect ratios of 0, 3, and 6. For the elliptical and rectangular wings the spanwise lift distributions were also presented. These functions were calculated from the lift coefficients associated with a wing oscillating harmonically in pure translational motion, as obtained from several sources.
Publisher:
ISBN:
Category : Air flow
Languages : en
Pages : 26
Book Description
The unsteady-lift functions for a wing undergoing a sudden change in sinking speed have been presented for delta wings having aspect ratios of 0, 2, and 4 and for rectangular and elliptical wings having aspect ratios of 0, 3, and 6. For the elliptical and rectangular wings the spanwise lift distributions were also presented. These functions were calculated from the lift coefficients associated with a wing oscillating harmonically in pure translational motion, as obtained from several sources.
Technical Note - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 480
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 480
Book Description
Technical Note
NASA Technical Note
Approximate indicial lift function for tapered, swept wings in incompressible flow
Author: M. J. Queijo
Publisher:
ISBN:
Category : Base flow (Aerodynamics)
Languages : en
Pages : 36
Book Description
Publisher:
ISBN:
Category : Base flow (Aerodynamics)
Languages : en
Pages : 36
Book Description
An Integral Equation Relating the General Time-dependent Lift and Downwash Distributions on Finite Wings in Subsonic Flow
Author: Joseph A. Drischler
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 32
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 32
Book Description
Correlation, Evaluation, and Extension of Linearized Theories for Tire Motion and Wheel Shimmy
Author: Robert F. Smiley
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 728
Book Description
A series of systematic approximations to the summary theory is developed for the treatment of problems too simple to merit the use of the complete summary theory, and procedures are discussed for applying the summary theory and its systematic approximations to the shimmy of more complex landing-gear structures than have previously been considered.
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 728
Book Description
A series of systematic approximations to the summary theory is developed for the treatment of problems too simple to merit the use of the complete summary theory, and procedures are discussed for applying the summary theory and its systematic approximations to the shimmy of more complex landing-gear structures than have previously been considered.
NASA Technical Paper
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 814
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 814
Book Description
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.
Unsteady Aerodynamic Forces on Subsonic Aircraft Exposed to Blast Gusts of Arbitrary Orientation
Author: Robert F. Smiley
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 108
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 108
Book Description