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Hypersonic slender body aerodynamics (Record no. 567666)

MARC details
000 -LEADER
fixed length control field 01663 a2200217 4500
003 - CONTROL NUMBER IDENTIFIER
control field OSt
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20250924150916.0
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 250924b |||||||| |||| 00| 0 eng d
020 ## - INTERNATIONAL STANDARD BOOK NUMBER
ISBN 9781394285631
082 ## - DEWEY DECIMAL CLASSIFICATION NUMBER
Classification number 629.132306
Item number R187h
100 ## - MAIN ENTRY--AUTHOR NAME
Personal name Rathakrishnan, Ethirajan
245 ## - TITLE STATEMENT
Title Hypersonic slender body aerodynamics
Statement of responsibility, etc Ethirajan Rathakrishnan
260 ## - PUBLICATION, DISTRIBUTION, ETC. (IMPRINT)
Name of publisher John Wiley
Year of publication 2025
Place of publication Hoboken
300 ## - PHYSICAL DESCRIPTION
Number of Pages xix, 179p
440 ## - SERIES STATEMENT/ADDED ENTRY--TITLE
Title Aerospace series
490 ## - SERIES STATEMENT
Series statement / edited by Peter Belobaba, Jonathan Cooper and Allan Seabridge
500 ## - GENERAL NOTE
General note with website.
520 ## - SUMMARY, ETC.
Summary, etc Developed using class-tested course material, Hypersonic Slender Body Aerodynamics presents the theoretical and application aspects of the subject in a precise, concise, and student-friendly manner. The text includes a large number of worked examples, figures, diagrams, tables, and exercise problems.<br/>This book covers the subject material beginning from the definition of the slender body geometry through to the study of flow field around the body and the calculation of the aerodynamic and thermal loads acting on the body at speeds ranging from low to high (i.e., from incompressible to hypersonic speeds). The Mach number independence principle and approximate theories for caret wings are also covered, among many other key topics.<br/>This book is unique in its comprehensive coverage of the topic, enabling readers to find information in one place instead of scattered throughout proprietary wind tunnel test data, flight test data, government technical reports, scientific literature sources, and numerical methods.
650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical Term Aerodynamics
-- Hypersonic slender body
942 ## - ADDED ENTRY ELEMENTS (KOHA)
Koha item type Books
Holdings
Withdrawn status Lost status Damaged status Not for loan Collection code Home library Current library Date acquired Source of acquisition Cost, normal purchase price Full call number Accession Number Cost, replacement price Koha item type
      Under Process General Stacks PK Kelkar Library, IIT Kanpur PK Kelkar Library, IIT Kanpur 24/09/2025 2 8938.35 629.132306 R187h A187060 11917.80 Books

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