Intake Aerodynamics
Blackwell Science Ltd (Publisher)
Published on 20. September 1999
Book
Hardback
432 pages
978-0-632-04963-9 (ISBN)
Description
This book provides a comprehensive, practical treatment of aerodynamics of supersonic intakes in both civil and military types of aircraft. The problems of both internal and external airflow are investigated. Simple mathematics are used only in analysis, and emphasis is placed on giving a physical picture of the flow, often with the aid of illustrations. The new edition takes account of the increase in computer based solutions of intake flow fields and correlates experimental work with results from computer programs.
More details
Edition
New edition
Language
English
Place of publication
Oxford
United Kingdom
Publishing group
John Wiley and Sons Ltd
Target group
College/higher education
Professional and scholarly
Edition type
New edition
Dimensions
Height: 244 mm
Width: 172 mm
Weight
1254 gr
ISBN-13
978-0-632-04963-9 (9780632049639)
Copyright in bibliographic data is held by Nielsen Book Services Limited or its licensors: all rights reserved.
Schweitzer Classification
Persons
Content
Introductory; Pressure Recovery of Subsonic Intakes; Transonic Effects in Pre-entry Flow; Lip Separation and Transonic Throat Flow; External Supersonic Compression; Internal Supersonic Compression; Additional Loss in Supersonic Intakes; Boundary Layer Bleeds and Diverters; Intake External Drag; Shock Oscillation of Supersonic Intakes; Distortion and Swirl; Matching and Control; Intakes at Incidence; Novel Designs and Devices; Techniques of Wind-Tunnel Testing and Analysis