TRANSSONISCHE PROFILE IM EXPERIMENT = PROFILS TRANSSONIQUES A L'ESSAISTANEWSKY E.1980; D.F.V.L.R.-NACHR.; DEU; DA. 1980; NO 30; PP. 34-40Article

Interaction between the outer inviscid flow and the boundary layer on transonic airfoilsSTANEWSKY, E.Zeitschrift für Flugwissenschaften und Weltraumforschung. 1983, Vol 7, Num 4, pp 242-252, issn 0342-068XArticle

ENTWICKLUNG UND WINDKANALERPROBUNG VON DREI UEBERKRITISCHEN TRAGFLUEGELPROFILEN FUER VERKEHRSFLUGZEUGE. = DEVELOPPEMENT ET EXPLORATION EN SOUFFLERIE DE TROIS PROFILS D'AILES SUPERCRITIQUES POUR AVIONS DE TRANSPORTSTANEWSKY E; ZIMMER H.1975; Z. FLUGWISSENSCH.; DTSCH.; DA. 1975; VOL. 23; NO 7-8; PP. 246-256; ABS. ANGL. FR.; BIBL. 14 REF.Article

HIGH-REYNOLDS NUMBER BOUNDARY-LAYER SHOCK-WAVE INTERACTION IN TRANSONIC FLOWSIRIEIX M; DELERY J; STANEWSKY E et al.1981; LECT. NOTES PHYS.; ISSN 0075-8450; DEU; DA. 1981; NO 148; PP. 149-214; BIBL. 23 REF.Conference Paper

THE COUPLING OF A SHOCK BOUNDARY LAYER INTERACTION MODULE WITH A VISCOUS-INVISCID COMPUTATION METHODSTANEWSKY E; NANDANAN M; INGER GR et al.1981; AGARD CONF. PROC.; ISSN 0549-7191; FRA; DA. 1981; NO 291; PP. 4.1-4.14; BIBL. 22 REF.Article

Boundary-layer transition on swept cylinders at hypersonic speedsMURAKAMI, A; STANEWSKY, E; KROGMANN, P et al.AIAA journal. 1996, Vol 34, Num 4, pp 649-654, issn 0001-1452Conference Paper

Effects of section on shock/boundary-layer interaction and shock-induced separationKROGMANN, P; STANEWSKY, E; THIEDE, P et al.Journal of aircraft. 1985, Vol 22, Num 1, pp 37-42, issn 0021-8669Article

Sidewall effects on airfoil testsGANZER, U; STANEWSKY, E; ZIEMANN, J et al.AIAA journal. 1984, Vol 22, Num 2, pp 297-299, issn 0001-1452Article

Drag reduction through control of shock boundary layer interactionSTANEWSKY, E; DELERY, J; FULKER, J et al.ECCOMAS computational fluid dynamics conferenceECCOMAS conference on numerical methods in engineering. 1996, pp 455-465, isbn 0-471-96226-0Conference Paper