FLOW COMPUTATION FOR THE HYPERSONIC CONFIGURATION ELAC-I AT LOW-SPEEDS AND LARGE INCIDENCE

Authors
MULLER CA BALLMANN J
Citation
Ca. Muller et J. Ballmann, FLOW COMPUTATION FOR THE HYPERSONIC CONFIGURATION ELAC-I AT LOW-SPEEDS AND LARGE INCIDENCE, Zeitschrift fur Flugwissenschaften und Weltraumforschung, 17(2), 1993, pp. 108-115
Citations number
NO
Categorie Soggetti
Aerospace Engineering & Tecnology
Journal title
Zeitschrift fur Flugwissenschaften und Weltraumforschung → ACNP
ISSN journal
0342068X
Volume
17
Issue
2
Year of publication
1993
Pages
108 - 115
Database
ISI
SICI code
0342-068X(1993)17:2<108:FCFTHC>2.0.ZU;2-6
Abstract
A combination of a higher order panel method and a second order bounda ry layer calculation is used for the analysis of the flow around gener ic hypersonic configurations. A new approach to simulate the flow sepa rating from smooth surfaces at low speeds and high incidence is presen ted. The essential elements of the method are discussed and the numeri cal technique is applied to the hypersonic configuration ELACI. Some r esults and a comparison with experiments are presented.