EXPERIMENTAL INVESTIGATION OF A GAS-DYNAMIC THRUST VECTOR CONTROL FORHYPERSONIC SPACE PLANES

Authors
ZEUTZIUS M BEYLICH AE MATSUO S SETOGUCHI T
Citation
M. Zeutzius et al., EXPERIMENTAL INVESTIGATION OF A GAS-DYNAMIC THRUST VECTOR CONTROL FORHYPERSONIC SPACE PLANES, JSME international journal. Series B, fluids and thermal engineering, 39(1), 1996, pp. 101-111
Citations number
11
Categorie Soggetti
Engineering, Mechanical",Thermodynamics
Journal title
JSME international journal. Series B, fluids and thermal engineering → ACNP
ISSN journal
13408054
Volume
39
Issue
1
Year of publication
1996
Pages
101 - 111
Database
ISI
SICI code
1340-8054(1996)39:1<101:EIOAGT>2.0.ZU;2-3
Abstract
The feasibility and performance of a gas dynamic thrust vector control for advanced space planes using wall bleeding were investigated exper imentally in the form of a parameter variation. In these studies, atte mpts were made to minimize the required control mass flows taken from the forebody boundary layer or intake. Furthermore, a semiempirical me thod for the design of the bleeding channel and geometry is presented, as well as a possible application of the results to flight mechanics.