Published May 2002
| public
Journal Article
Hypersonic flow over bodies in tandem
- Creators
-
Hornung, H. G.
Chicago
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Abstract
A computational study of hypersonic flow over two bodies in tandem was made with the aim to understand the problems that may be encountered when the drag of a ballute is used to decelerate a spacecraft in the outer atmosphere of a planet for aerocapture. When the trailing body is large, shock-shock interaction causes the flow to become violently unsteady. This can be avoided by making the second body in the shape of a ring. Several configurations are examined, and the interesting phenomena that occur are discussed.
Additional Information
© 2002 Springer Verlag. Received 27 July 2001 / Accepted 8 February 2002. An abridged version of this paper was presented at the 23rd Int. Symposium on Shock Waves at Fort Worth, Texas, from July 22 to 27, 2001.Additional details
- Eprint ID
- 101385
- Resolver ID
- CaltechAUTHORS:20200219-114918491
- Created
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2020-02-19Created from EPrint's datestamp field
- Updated
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2021-11-16Created from EPrint's last_modified field
- Caltech groups
- GALCIT