Loughborough University
Leicestershire, UK
LE11 3TU
+44 (0)1509 263171
Loughborough University

Loughborough University Institutional Repository

Please use this identifier to cite or link to this item: https://dspace.lboro.ac.uk/2134/8031

Title: Maneuver of fixed-wing combat aircraft
Authors: Render, Peter M.
Issue Date: 2010
Publisher: © John Wiley and Sons, Inc.
Citation: RENDER, P.M., 2010. Maneuver of fixed-wing combat aircraft. IN: Blockley, R., Shyy, W. (eds.). Encyclopedia of Aerospace Engineering. John Wiley and Sons, Inc.
Abstract: Introduction: The ability to maneuver is an important consideration for fixed wing combat aircraft and is required for both aggressive and evasive maneuvers. Small differences in maneuver performance can be significant in determining which aircraft will win a combat engagement. For example, pilots often regard a difference of 2–3◦ s−1 in turn rate as being significant. The required maneuver performance will be determined by the aircraft’s role. For instance, an air combat aircraft designed to engage enemy fighters is likely to require high instantaneous turn rates, whilst a beyond visual range interceptor armed with long range missiles is more likely to be concerned with acceleration at high altitude and good climb to height characteristics.
Description: This book chapter is posted with special permission of John Wiley & Sons Ltd., granted to the author on 1st April 2009. Further details of this book are available at: http://onlinelibrary.wiley.com/book/10.1002/9780470686652
Version: Published (Proof)
DOI: 10.1002/9780470686652
URI: https://dspace.lboro.ac.uk/2134/8031
Publisher Link: http://dx.doi.org/10.1002/9780470686652.eae249
http://dx.doi.org/10.1002/9780470686652
ISBN: 9780470686652
9780470754405
0470754400
Appears in Collections:Book Chapters (Aeronautical and Automotive Engineering)

Files associated with this item:

File Description SizeFormat
EncyclopaediaFinal_Proofeae249.pdf444.14 kBAdobe PDFView/Open

 

SFX Query

Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.