THE EFFECT OF SWEEP ON CONDITIONS AT SEPERATION IN TURBULENT BOUNDARY-LAYER/SHOCK-WAVE INTERACTION.MYRING DF.1977; AERONAUT. QUART.; G.B.; DA. 1977; VOL. 28; NO 2; PP. 111-122; BIBL. 15 REF.Article

PRESSURE RISE TO SEPARATION IN CYLINDRICALLY SYMMETRIC SHOCK WAVE-TURBULENT BOUNDARY LAYER INTERACTION. = HAUSSE DE LA PRESSION DU DECOLLEMENT DANS L'INTERACTION ONDE DE CHOC A SYMETRIE CYLINDRIQUE-COUCHE LIMITE TURBULENTEMYRING DF.1975; A.G.A.R.D. CONF. PROC.; FR.; DA. 1975; NO 168; PP. (14P.); BIBL. 1 P. 1/2; (FLOW SEP. FLUID DYN. PANEL SYMP.; GOTTINGEN, GER.; 1975)Conference Paper