Approximate Indicial Lift Functions for Several Wings of Finite Span in Incompressible Flow as Obtained from Oscillatory Lift Coefficients PDF Download

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Approximate Indicial Lift Functions for Several Wings of Finite Span in Incompressible Flow as Obtained from Oscillatory Lift Coefficients

Approximate Indicial Lift Functions for Several Wings of Finite Span in Incompressible Flow as Obtained from Oscillatory Lift Coefficients PDF 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

Approximate Indicial Lift Functions for Several Wings of Finite Span in Incompressible Flow as Obtained from Oscillatory Lift Coefficients PDF 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.

Technical Note - National Advisory Committee for Aeronautics

Technical Note - National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 480

Book Description


Technical Note

Technical Note PDF Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 568

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NASA Technical Note

NASA Technical Note PDF Author:
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Category :
Languages : en
Pages : 694

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Approximate indicial lift function for tapered, swept wings in incompressible flow

Approximate indicial lift function for tapered, swept wings in incompressible flow PDF Author: M. J. Queijo
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

An Integral Equation Relating the General Time-dependent Lift and Downwash Distributions on Finite Wings in Subsonic Flow PDF Author: Joseph A. Drischler
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 32

Book Description


Correlation, Evaluation, and Extension of Linearized Theories for Tire Motion and Wheel Shimmy

Correlation, Evaluation, and Extension of Linearized Theories for Tire Motion and Wheel Shimmy PDF 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.

NASA Technical Paper

NASA Technical Paper PDF Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 814

Book Description


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Principles of Aeroelasticity PDF 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.

Unsteady Aerodynamic Forces on Subsonic Aircraft Exposed to Blast Gusts of Arbitrary Orientation

Unsteady Aerodynamic Forces on Subsonic Aircraft Exposed to Blast Gusts of Arbitrary Orientation PDF Author: Robert F. Smiley
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 108

Book Description