Theoretical Span Load Distributions and Rolling Moments for Sideslipping Wings of Arbitrary Plan Form in Incompressible Flow

Theoretical Span Load Distributions and Rolling Moments for Sideslipping Wings of Arbitrary Plan Form in Incompressible Flow
Author :
Publisher :
Total Pages : 54
Release :
ISBN-10 : UOM:39015086430033
ISBN-13 :
Rating : 4/5 (33 Downloads)

Book Synopsis Theoretical Span Load Distributions and Rolling Moments for Sideslipping Wings of Arbitrary Plan Form in Incompressible Flow by : M. J. Queijo

Download or read book Theoretical Span Load Distributions and Rolling Moments for Sideslipping Wings of Arbitrary Plan Form in Incompressible Flow written by M. J. Queijo and published by . This book was released on 1955 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt: A method of computing span loads and the resulting rolling moments for sideslipping wings of arbitrary plan form in incompressible flow is derived. The method requires that the span load at zero sideslip be known for the wing under consideration. Because this information is available for a variety of wings, this requirement should not seriously restrict the application of the present method. The basic method derived herein requires a mechanical differentiation and integration to obtain the rolling moment for the general wing in sideslip. For wings having straight leading and trailing edges over each semispan, the rolling moment equation in terms of plan-form parameters and the lateral center of pressure of the lift due to angle of attack. Calculated span loads and rolling-moment parameters are compared with experimental values. The comparison indicates good agreement between calculations and available experimental data.


Theoretical Span Load Distributions and Rolling Moments for Sideslipping Wings of Arbitrary Plan Form in Incompressible Flow Related Books

Theoretical Span Load Distributions and Rolling Moments for Sideslipping Wings of Arbitrary Plan Form in Incompressible Flow
Language: en
Pages: 54
Authors: M. J. Queijo
Categories: Aerodynamic load
Type: BOOK - Published: 1955 - Publisher:

DOWNLOAD EBOOK

A method of computing span loads and the resulting rolling moments for sideslipping wings of arbitrary plan form in incompressible flow is derived. The method r
Report
Language: en
Pages: 22
Authors: United States. National Advisory Committee for Aeronautics
Categories: Aeronautics
Type: BOOK - Published: 1953 - Publisher:

DOWNLOAD EBOOK

Integrated Vehicle Dynamics and Control
Language: en
Pages: 370
Authors: Wuwei Chen
Categories: Technology & Engineering
Type: BOOK - Published: 2016-05-31 - Publisher: John Wiley & Sons

DOWNLOAD EBOOK

A comprehensive overview of integrated vehicle system dynamics exploring the fundamentals and new and emerging developments This book provides a comprehensive c
NASA Technical Note
Language: en
Pages: 1068
Authors:
Categories: Aeronautics
Type: BOOK - Published: 1964 - Publisher:

DOWNLOAD EBOOK

Introduction to Avionics Systems
Language: en
Pages: 341
Authors: R.P.G. Collinson
Categories: Technology & Engineering
Type: BOOK - Published: 2023-06-01 - Publisher: Springer Nature

DOWNLOAD EBOOK

Now in a revised fourth edition, this course-tested textbook explains the basic principles and underlying theory of the core avionic systems in modern civil and