Sustained hypersonic flight using scramjet propulsion is the key
technology bridging the gap between turbojets and the
exoatmospheric environment where a rocket is required. Recent
efforts have focused on electromagnetic (EM) flow control to
mitigate the problems of high thermomechanical loads and low
propulsion efficien- cies associated with scramjet propulsion. This
research effort is the first flight-scale, three-dimensional
computational analysis of a realistic scramjet to determine how EM
flow control can improve scramjet performance. Development of a
quasi-one dimen- sional design tool culminated in the first open
source geometry of an entire scramjet flowpath. This geometry was
then tested extensively with the Air Force Research Laboratory's
three-dimensional Navier-Stokes and EM coupled computational code.
General
Imprint: |
Biblioscholar
|
Country of origin: |
United States |
Release date: |
November 2012 |
First published: |
November 2012 |
Authors: |
Martin Forrester Lindsey
|
Dimensions: |
246 x 189 x 10mm (L x W x T) |
Format: |
Paperback - Trade
|
Pages: |
180 |
ISBN-13: |
978-1-288-33513-8 |
Categories: |
Books >
Social sciences >
Education >
General
|
LSN: |
1-288-33513-X |
Barcode: |
9781288335138 |
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