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
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.