An Integrated Approach To The Analysis And Design Of Wings And Wing Body Combinations In Supersonic Flow PDF Download

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A Method for Calculating the Aerodynamic Loading on Wing-body Combinations at Small Angles of Attack in Supersonic Flow

A Method for Calculating the Aerodynamic Loading on Wing-body Combinations at Small Angles of Attack in Supersonic Flow
Author: Charlie M. Jackson
Publisher:
Total Pages: 44
Release: 1971
Genre: Aerodynamics, Supersonic
ISBN:

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This report describes a theoretical method for estimating the aerodynamic loading on a wing-body configuration. In order to provide a basis for evaluation of the method, experimental measurements of surface pressures, forces, and moments were made on a series of basic wing-body configurations over a Mach number range from 2.5 to 4.5. Comparison of the theoretical estimates with these experimental data generally indicated good agreement for the entire range of configurations and test conditions.


Applied Mechanics Reviews

Applied Mechanics Reviews
Author:
Publisher:
Total Pages: 636
Release: 1973
Genre: Mechanics, Applied
ISBN:

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Aerodynamics for Engineers

Aerodynamics for Engineers
Author: John J. Bertin
Publisher: Cambridge University Press
Total Pages: 843
Release: 2021-08-12
Genre: Technology & Engineering
ISBN: 1009115758

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Now reissued by Cambridge University Press, this sixth edition covers the fundamentals of aerodynamics using clear explanations and real-world examples. Aerodynamics concept boxes throughout showcase real-world applications, chapter objectives provide readers with a better understanding of the goal of each chapter and highlight the key 'take-home' concepts, and example problems aid understanding of how to apply core concepts. Coverage also includes the importance of aerodynamics to aircraft performance, applications of potential flow theory to aerodynamics, high-lift military airfoils, subsonic compressible transformations, and the distinguishing characteristics of hypersonic flow. Supported online by a solutions manual for instructors, MATLAB® files for example problems, and lecture slides for most chapters, this is an ideal textbook for undergraduates taking introductory courses in aerodynamics, and for graduates taking preparatory courses in aerodynamics before progressing to more advanced study.


NASA Technical Note

NASA Technical Note
Author:
Publisher:
Total Pages: 508
Release: 1971
Genre:
ISBN:

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Store Separation

Store Separation
Author: Bertha M. Ryan
Publisher:
Total Pages: 82
Release: 1973
Genre: Weapons systems
ISBN:

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