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Aerodynamic principles of flight vehicles

Author: A G Panaras
Publisher: Reston, VA : American Institute of Aeronautics and Astronautics, [2012] ©2012
Series: Library of flight.
Edition/Format:   eBook : Document : EnglishView all editions and formats
Summary:
This book examines the fundamentals of vortices and shock waves, aerodynamic estimation of lift and drag, airfoil theory, boundary layer control, and high-speed, high-temperature flow. Individual chapters address vortices in aerodynamics, transonic and supersonic flows, transonic/supersonic aircraft configurations, and high-supersonic/hypersonic flows, beginning with definitions and historical data, and then  Read more...
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Genre/Form: Electronic books
Additional Physical Format: Print version:
Panaras, A.G.
Aerodynamic principles of flight vehicles
(DLC) 2012020128
(OCoLC)795173209
Material Type: Document, Internet resource
Document Type: Internet Resource, Computer File
All Authors / Contributors: A G Panaras
ISBN: 9781628701555 1628701552 9781600869174 1600869173
OCLC Number: 871686733
Description: 1 online resource (xiii, 319 pages) : illustrations.
Contents: ""Cover""; ""Title""; ""Copyright""; ""A Note from the Editor-in-Chief""; ""Table of Contents""; ""Preface""; ""Acknowledgements""; ""Chapter 1. Introduction""; ""Chapter 2. Vortices in Aerodynamics""; ""Chapter 3. Transonic and Supersonic Flows""; ""Chapter 4. Transonic Aircraft Configurations""; ""Chapter 5. High-Supersonic/Hypersonic Flows""; ""Appendix: Analysis of Fundamental Relations and Theorems""; ""Index""; ""Supporting Materials""
Series Title: Library of flight.
Responsibility: Argyris G. Panaras.

Abstract:

This book examines the fundamentals of vortices and shock waves, aerodynamic estimation of lift and drag, airfoil theory, boundary layer control, and high-speed, high-temperature flow. Individual chapters address vortices in aerodynamics, transonic and supersonic flows, transonic/supersonic aircraft configurations, and high-supersonic/hypersonic flows, beginning with definitions and historical data, and then describing present-day status and current research challenges. Emphasis is given to flow control, the evolution of flight vehicle shapes as flight speed has increased, and discoveries that enabled breakthrough developments in flight. The book examines why various equations and technologies were developed; explains major contributors in areas such as vortices and aircraft wakes, drag buildup, sonic boom, and shock wave/boundary layer interactions, among others; and helps readers apply concepts from the material to their own projects. This resource is for both aeronautical students and professionals. --

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