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This comprehensive reference brings together all available
information that has been generated over time, through general
research investigations and studies of specific configurations, on
the aerodynamic effects induced by the exiting flows of jet and fan
powered V/STOL aircraft in hover and transition flight.
Written by several of the foremost authorities in the field, here
for the first time is an all-inclusive compilation of existing
experimental data along with in-depth discussions on jet
interference effects. For the working professional or those in
engineering graduate programs, especially those involved with
V/STOL, this book will prove an invaluable resource. It also
provides the researcher with a starting point for future
investigations that could be applied to new aircraft development
programs.
The unique characteristics of V/STOL flight bring with it unique
aerodynamic challenges. This book describes the flow fields
generated by the mixing of exit flows with surrounding and free
stream air and their effects on the aircraft and the surrounding
environment.
These flows have differing effects depending on the aircraft
configuration and on whether the aircraft is in hover or
transitional flight. The aerodynamic/propulsion interactions affect
the total lift, drag, and pitching moments, effectiveness of jet
reaction control jets, ground effects, thrust loss, landing surface
damage, and effects on the operational environment. Each of these
issues is fully presented, illustrated, and discussed in
detail.
In addition, a chapter is devoted to present and future efforts in
V/STOL research and how it relates to developing Computational
Fluid Dynamics (CFD) methods for analyzing and estimating the flow
fields around these aircraft and their effects.
Each of the book’s chapters includes an extensive list of
references from which the material in that chapter is derived.
| Product Code |
Description |
Attributes |
Price | |
| ISBN: 9781563478413 Richard Kuhn |
Hardback 2007 |
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£69.00
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0% VAT
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