Aerospace Engineering e-Mega Reference

Aerospace Engineering e-Mega Reference

by Tooley, Mike

Type Book
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A one-stop Desk Reference, for engineers involved in all aspects of aerospace; this is a book that will not gather dust on the shelf. It brings together the essential professional reference content from leading international contributors in the field. Material covers a broad topic range from Structural Components of Aircraft, Design and Airworthiness to Aerodynamics and Modelling* A fully searchable Mega Reference Ebook, providing all the essential material needed by Aerospace Engineers on a da…

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Title Statements

  • Full title :Aerospace Engineering e-Mega Reference.

Summary

A one-stop Desk Reference, for engineers involved in all aspects of aerospace; this is a book that will not gather dust on the shelf. It brings together the essential professional reference content from leading international contributors in the field. Material covers a broad topic range from Structural Components of Aircraft, Design and Airworthiness to Aerodynamics and Modelling* A fully searchable Mega Reference Ebook, providing all the essential material needed by Aerospace Engineers on a day-to-day basis. * Fundamentals, key techniques, engineering best practice and rule.

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Edition Statements

  • Publication Date:2009.

Publication Statements

  • Publisher(s):Elsevier Science
  • Place of Publication:Burlington
  • Language:eng
  • Publication Date:2009.

Notes

4.1.4 Aircraft Equations of Motion.

The Physical Object

  • Description:1 online resource (687 pages)

Edition Identifiers

  • ISBN:1856175758, 9781856175753
  • oclc:ocn990451879
  • LC Classification:TL501
  • Dewey Decimal:629.1

Table of Contents

Front Cover; Note from the Publisher; Aerospace Engineering Desk Reference; Copyright Page; Contents; Author Biographies; Section 1 Introduction; Chapter 1.0 Introduction; 1.1 Physical Units Used; 1.2 Performance Parameters; 1.3 Performance Optimization; 1.4 Certificate of Airworthiness; 1.5 Upgrading of Aircraft Performance; 1.6 Mission Profiles; Section 2 Flight Performance; Chapter 2.1 The Aircraft and its Environment; 2.1.1 General Aircraft Model; 2.1.2 Reference Systems; 2.1.3 Forces on the Aircraft; 2.1.4 Moments of Inertia; 2.1.5 Flight Dynamics Equations.

2.1.6 The International Standard Atmosphere2.1.7 Non-Standard Conditions; Chapter 2.2 Weight; 2.2.1 The Aircraft's Weight; 2.2.2 Definition of Weights; 2.2.3 Weight Estimation; 2.2.4 Weight Management; 2.2.5 Range/Payload Diagram; 2.2.6 Direct Operating Costs; Chapter 2.3 Aerodynamics; 2.3.1 Aerodynamic Forces; 2.3.2 Lift Equation; 2.3.3 Vortex Lift; 2.3.4 High-Lift Systems; 2.3.5 Drag Equation; 2.3.6 Glide Ratio; 2.3.7 Glide Ratio at Transonic and Supersonic Speed; 2.3.8 Practical Estimation of the Drag Coefficient; 2.3.9 Compressibility Effects; 2.3.10 Transonic Drag Rise.

2.3.11 Lift and Transonic Buffet2.3.12 Aero-T…

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