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A TURBULENCE MODEL NONEQUILIBRIUM ADVERSE PRESSURE GRADIENT FLOWS.HORSTMAN CC.1976; IN: FLUID PLASMA DYN. CONF. 9; SAN DIEGO, CALIF.; 1976; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. 1976; VOL. 412; PP. 1-11; BIBL. 28 REF.Conference Paper

TURBULENCE MODEL FOR NONEQUILIBRIUM ADVERSE PRESSURE GRADIENT FLOWS.HORSTMAN CC.1977; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1977; VOL. 15; NO 2; PP. 131-132; BIBL. 9 REF.Article

TURBULENCE STRESS MEASUREMENTS IN A NONADIABATIC HYPERSONIC BOUNDARY LAYER.MIKULLA V; HORSTMAN CC.1975; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 12; PP. 1607-1613; BIBL. 10 REF.Article

NEW DIAGNOSTIC TECHNIQUE FOR THE STUDY OF TURBULENT BOUNDARY-LAYER SEPARATION.HORSTMAN CC; OWEN FK.1974; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1974; VOL. 12; NO 10; PP. 1437-1438; BIBL. 4 REF.Article

COMPARISON OF MULTIEQUATION TURBULENCE MODELS FOR SEVERAL SHOCK BOUNDARY-LAYER INTERACTION FLOWSVIEGAS JR; HORSTMAN CC.1979; A.I.A.A.J., NEW YORK; USA; DA. 1979; VOL. 17; NO 8; PP. 811-820; BIBL. 29 REF.Article

TURBULENCE MEASUREMENTS IN HYPERSONIC SHOCK-WAVE BOUNDARY-LAYER INTERACTION FLOWS.MIKULLA V; HORSTMAN CC.1976; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1976; VOL. 14; NO 5; PP. 568-575; BIBL. 10 REF.Article

REYNOLDS NUMBER AND PRESSURE GRADIENT EFFECTS ON COMPRESSIBLE TURBULENT BOUNDARY LAYERSACHARYA M; KUSSOY MI; HORSTMAN CC et al.1978; A.I.A.A.J., NEW YORK; USA; DA. 1978; VOL. 16; NO 12; PP. 1217-1218; BIBL. 6 REF.Article

MEAN AND FLUCTUATING FLOW MEASUREMENTS OF A FULLY-DEVELOPED, NON-ADIABATIC, HYPERSONIC BOUNDARY LAYER.OWEN FK; HORSTMAN CC; KUSSOY MI et al.1975; J. FLUID MECH.; G.B.; DA. 1975; VOL. 70; NO 2; PP. 393-413; BIBL. 18 REF.Article

COMPARISON OF TRANSITION AND FREESTREAM DISTURBANCE MEASUREMENTS OBTAINED IN TWO WIND TUNNEL FACILITIES.OWEN FK; HORSTMAN CC; STAINBACK PC et al.1974; IN: AM. INST. AERONAUT. ASTRONAUT. AEROSP. SCI. MEET.; WASHINGTON; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 131; PP. 1-4; BIBL. 7 REF.Conference Paper

TRAILING-EDGE FLOWS AT HIGH REYNOLDS NUMBERVISWANATH PR; CLEARY JW; SEEGMILLER HL et al.1980; AIAA J.; ISSN 0001-1452; USA; DA. 1980; VOL. 18; NO 9; PP. 1059-1065; BIBL. 22 REF.Article

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

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