SOME REMARKS ON SHOCK WAVE TURBULENT BOUNDARY-LAYER INTERACTION AT HIGH REYNOLDS NUMBER.BOGDONOFF SM.1975; S.I.A.M. J. APPL. MATH.; U.S.A.; DA. 1975; VOL. 29; NO 2; PP. 293-308; BIBL. 17 REF.Article

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SCALING OF INTERACTIONS OF CYLINDERS WITH SUPERSONIC TURBULENT BOUNDARY LAYERSDOLLING DS; BOGDONOFF SM.1981; AIAA J.; ISSN 0001-1452; USA; DA. 1981; VOL. 19; NO 5; PP. 655-657; BIBL. 16 REF.Article

DETAILED STUDY OF ATTACHED AND SEPARATED COMPRESSION CORNER FLOWFIELDS IN HIGH REYNOLDS NUMBER SUPERSONIC FLOWSETTLES GS; FITZPATRICK TJ; BOGDONOFF SM et al.1979; A.I.A.A. J., NEW YORK; USA; DA. 1979; VOL. 17; NO 6; PP. 579-585; BIBL. 23 REF.Article

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INVESTIGATION OF THREE-DIMENSIONAL SHOCK/BOUNDARY-LAYER INTERACTIONS AT SWEPT COMPRESSION CORNERSSETTLES GS; PERKINS JJ; BOGDONOFF SM et al.1980; AIAA J.; ISSN 0001-1452; USA; DA. 1980; VOL. 18; NO 7; PP. 779-785; BIBL. 20 REF.Article

INCIPIENT SEPARATION OF A SUPERSONIC TURBULENT BOUNDARY LAYER AT HIGH REYNOLDS NUMBERS.SETTLES GS; BOGDONOFF SM; VAS IE et al.1976; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1976; VOL. 14; NO 1; PP. 50-56; BIBL. 22 REF.Article

MACH 3 OBLIQUE SHOCK WAVE-TURBULENT BOUNDARY LAYER INTERACTIONS IN THREE DIMENSIONS.OSKAM B; VAS IE; BOGDONOFF SM et al.1976; IN: FLUID PLASMA DYN. CONF. 9; SAN DIEGO, CALIF.; 1976; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. 1976; VOL. 336; PP. 1-19; BIBL. 1 P. 1/2Conference Paper

A REATTACHING FREE SHEAR LAYER IN COMPRESSIBLE TURBULENT FLOW: A COMPARISON OF NUMERICAL AND EXPERIMENTAL RESULTSHORTSMAN CC; SETTLES GS; WILLIAMS DR et al.1981; AEROSPACE SCIENCES MEETING. 19 /1981-01-12/SAINT LOUIS MO; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1981; 10 P.; BIBL. 16 REF.Conference Paper

A REATTACHING FREE SHEAR LAYER IN COMPRESSIBLE TURBULENT FLOWHORSTMAN CC; SETTLES GS; WILLIAMS DR et al.1981; AIAA J.; ISSN 0001-1452; USA; DA. 1981; VOL. 20; NO 1; PP. 79-85; BIBL. 16 REF.Article

REYNOLDS NUMBER EFFECTS ON SHOCK-WAVE TURBULENT BOUNDARY-LAYER INTERACTIONS.HORSTMAN CC; SETTLES GS; VAS IE et al.1977; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1977; VOL. 15; NO 8; PP. 1152-1158; BIBL. 18 REF.Article

AN EXPLORATORY STUDY OF A THREE-DIMENSIONAL SHOCK WAVE BOUNDARY LAYER INTERACTION AT MACH 3. = ETUDE EXPLORATOIRE D'UNE INTERACTION ONDE DE CHOC TRIDIMENSIONNELLE-COUCHE LIMITE A MACH 3OSKAM B; VAS IE; BOGDONOFF SM et al.1975; A.G.A.R.D. CONF. PROC.; FR.; DA. 1975; NO 168; PP. 41.1-41.14; BIBL. 13 REF.; (FLOW SEP. FLUID DYN. PANEL SYMP.; GOTTINGEN, GER.; 1975)Conference Paper