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THE VERTICAL PLATE IN LAMINAR FREE CONVECTION: EFFECTS OF LEADING AND TRAILING EDGES AND DISCONTINUOUS TEMPERATURE.MESSITER AF.1976; Z. ANGEW. MATH. PHYS.; SCHWEIZ; DA. 1976; VOL. 27; NO 5; PP. 633-651; ABS. ALLEM.; BIBL. 20 REF.Article

LAMINAR SEPARATION. A LOCAL ASYMPTOTIC FLOW DESCRIPTION FOR CONSTANT PRESSURE DOWNSTREAM. = DECOLLEMENT LAMINAIRE. DESCRIPTION DE L'ECOULEMENT ASYMPTOTIQUE LOCAL POUR UNE PRESSION A L'AVAL CONSTANTEMESSITER AF.1975; A.G.A.R.D. CONF. PROC.; FR.; DA. 1975; NO 168; PP. 4.1-4.10; BIBL. 22 REF.; (FLOW SEP. FLUID DYN. PANEL SYMP.; GOETTINGEN, GER.; 1975)Conference Paper

BOUNDARY-LAYER SEPARATIONMESSITER AF.1979; UNITED STATES NATIONAL CONGRESS OF APPLIED MECHANICS. 8/1978/LOS ANGELES CA; USA; NORTH HOLLYWOOD CA: WESTERN PERIODICALS; DA. 1979; PP. 157-179; BIBL. 98 REF.Conference Paper

BOUNDARY-LAYER EFFECTS ON THE REFLECTION OF SOUND WAVES AND WEAK SHOCK WAVES AT SHALLOW INCIDENCE.MESSITER AF.1977; Z. ANGEW. MATH. PHYS.; SCHWEIZ; DA. 1977; VOL. 28; NO 5; PP. 879-887; ABS. ALLEM.; BIBL. 3 REF.Article

INTERACTION BETWEEN A NORMAL SHOCK WAVE AND A TURBULENT BOUNDARY LAYER AT HIGH TRANSONIC SPEEDS. I: PRESSURE DISTRIBUTIONMESSITER AF.1980; Z. ANGEW. MATH. PHYS.; CHE; DA. 1980; VOL. 31; NO 2; PP. 204-226; ABS. GER; BIBL. 32 REF.Article

A MODEL FOR LAMINAR BOUNDARY LAYER FLOW NEAR A SEPARATION POINT.MESSITER AF; ENLOW RL.1973; S.I.A.M. J. APPL. MATH.; U.S.A.; DA. 1973; VOL. 25; NO 4; PP. 655-670; BIBL. 20 REF.Article

ON THE FLOW NEAR A WEAK SHOCK WAVE DOWNSTREAM OF A NOZZLE THROAT.MESSITER AF; ADAMSON TC.1975; J. FLUID MECH.; G.B.; DA. 1975; VOL. 69; NO 1; PP. 97-108; BIBL. 7 REF.Article

LAMINAR BOUNDARY LAYER AT A DISCONTINUITY IN WALL CURVATURE.MESSITER AF; HU JJ.1975; QUART. APPL. MATH.; U.S.A.; DA. 1975; VOL. 33; NO 2; PP. 175-181; BIBL. 6 REF.Article

ANALYSIS OF TWO-DIMENSIONAL INTERACTION BETWEEN SHOCK WAVES AND BOUNDARY LAYERSADAMSON TC JR; MESSITER AF.1980; ANNU. REV. FLUID MECH.; USA; DA. 1980; VOL. 12; PP. 103-138; BIBL. 5 P.Article

SIMPLE APPROXIMATIONS FOR THE ASYMPTOTIC DESCRIPTION OF THE INTERACTION BETWEEN A NORMAL SHOCK WAVE AND A TURBULENT BOUNDARY LAYER AT TRANSONIC SPEEDSADAMSON TC JR; MESSITER AF.1981; AGARD CONF. PROC.; ISSN 0549-7191; FRA; DA. 1981; NO 291; PP. 16.1-16.14; BIBL. 23 REF.Article

TRANSONIC SMALL-DISTURBANCE THEORY FOR LIGHTLY LOADED CASCADESMESSITER AF; ADAMSON TC JR.1981; AIAA J.; ISSN 0001-1452; USA; DA. 1981; VOL. 19; NO 8; PP. 1047-1054; BIBL. 18 REF.Article

ON THE MATCHING OF SOLUTIONS FOR UNSTEADY TRANSONIC NOZZLE FLOWS.ADAMSON TC JR; MESSITER AF; RICHEY GK et al.1974; ARCH. MECH.; POLAND; DA. 1974; VOL. 26; NO 4; PP. 617-628; ABS. POL. RUSSE; BIBL. 9 REF.Article

LARGE AMPLITUDE SHOCK-WAVE MOTION IN TWO-DIMENSIONAL, TRANSONIC CHANNEL FLOWSADAMSON TC; MESSITER AF; LIOU MS et al.1978; A.I.A.A.J., NEW YORK; USA; DA. 1978; VOL. 16; NO 12; PP. 1240-1247; BIBL. 5 REF.Article

LARGE AMPLITUDE SHOCK WAVE MOTION IN TWO DIMENSIONAL TRANSONIC CHANNEL FLOWADAMSON TC JR; MESSITER AF; LIOU MS et al.1978; AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS AEROSPACE SCIENCES MEETING. 16/1978/HUNTSVILLE AL; USA; NEW YORK: AIAA; DA. 1978; 78-247; 8 P.; BIBL. 5 REF.Conference Paper

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