A SURVEY OF TRANSONIC AERODYNAMICS.WU JM; MOULDEN TH.1976; IN: FLUID PLASMA DYN. CONF. 9; SAN DIEGO, CALIF.; 1976; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. 1976; VOL. 326; PP. 1-37; BIBL. 9 P. 1/2Conference Paper

COMPUTATION OF TRANSONIC FLOW ABOUT LIFTING WING-CYLINDER COMBINATIONS.KLUNKER EB; NEWMAN PA.1974; J. AIRCR.; U.S.A.; DA. 1974; VOL. 11; NO 4; PP. 254-256; BIBL. 16 REF.Article

ESSAIS DE TREMBLEMENT ("BUFFETING") D'UNE AILE EN FLECHE EN TRANSSONIQUE.MONNERIE B; CHARPIN F.1975; AERONAUT. ET ASTRONAUT.; FR.; DA. 1975; NO 50; PP. 3-16; ABS. ANGL. ALLEM.; BIBL. 4 REF.Article

ITERATIVE SOLUTION OF TRANSONIC FLOWS OVER AIRFOILS AND WINGS, INCLUDING FLOWS AT MACH 1.JAMESON A.1974; COMMUNIC. PURE APPL. MATH.; U.S.A.; DA. 1974; VOL. 27; NO 3; PP. 283-309; BIBL. 20 REF.Article

TRANSONIC FLOW ABOUT LIFTING WING-BODY COMBINATIONS.BARNWELL RW.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 12TH AEROSP. SCI. MEET.; WASHINGTON; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 185; PP. 1-13; H.T. 2; BIBL. 16 REF.Conference Paper

HYBRIDTECHNIK ZUR ERZEUGUNG TRANSSONISCHER HOHER REYNOLDSZAHL. = TECHNIQUE HYBRIDE POUR LA PRODUCTION DE NOMBRES DE REYNOLDS TRANSSONIQUES ELEVESHOTTNER T.1974; Z. FLUGWISSENSCH.; DTSCH.; DA. 1974; VOL. 22; NO 12; PP. 403-416; ABS. ANGL. FR.; BIBL. 10 REF.Article

TRANSONIC INVISCID FLOW OVER LIFTING AIRFOILS BY THE METHOD OF INTEGRAL RELATIONS.TSZE CHENG TAI.1974; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1974; VOL. 12; NO 6; PP. 798-804; BIBL. 36 REF.Article

TRANSONIC LAMINAR VISCOUS-INVISCID INTERACTION OVER AIRFOILS.TAI TC.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 7TH FLUID PLASMA DYN. CONF.; PALO ALTO, CALIF.; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 600; PP. 1-11; BIBL. 29 REF.Conference Paper

AXISYMMETRIC SONIC FLOW COMPUTED BY A NUMERICAL METHOD APPLIED TO SLENDER BODIES.SEDIN YCJ.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 7TH FLUID PLASMA DYN. CONF.; PALO ALTO, CALIF.; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 544; PP. 1-12; BIBL. 16 REF.Conference Paper

EVALUATION OF DRAG INTEGRAL USING CUBIC SPLINES.JAMES RM; PANICO VD.1974; J. AIRCR.; U.S.A.; DA. 1974; VOL. 11; NO 8; PP. 494-496; BIBL. 4 REF.Article

OSCILLATIONS A BASSE FREQUENCE D'UN PROFIL EPAIS DANS UN ECOULEMENT TRANSSONIQUESYIGALOV GF.1974; DOP. AKAD. NAUK U.R.S.R., A; S.S.S.R.; DA. 1974; VOL. 36; NO 9; PP. 825-829; ABS. ANGL. RUSSE; BIBL. 6 REF.Article

SUR L'ECOULEMENT A VITESSE TRANSSONIQUE AUTOUR D'UN CORPS DE REVOLUTION AVEC UN CANAL DONNANT PASSAGE A UN JETKRAJKO AN; TAGIROV RK.1974; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1974; NO 6; PP. 73-80; BIBL. 8 REF.Article

THE STABILIZATION LAW FOR TRANSONIC FLOW.DIESPEROV WN; LIFSHITZ YU B; RYZHOV OS et al.1974; ARCH. MECH.; POLAND; DA. 1974; VOL. 26; NO 3; PP. 511-521; ABS. POL. RUSSE; BIBL. 13 REF.; (XITH SYMP. ADV. PROBL. METHODS FLUID MECH.; KAMIENNY POTOK, POL.; 1973)Conference Paper

INVISCID DRAG AT TRANSONIC SPEEDS.MURMAN EM; COLE JD.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 7TH FLUID PLASMA DYN. CONF.; PALO ALTO, CALIF.; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 540; PP. 1-15; BIBL. 19 REF.Conference Paper

NUMERICAL CALCULATION OF THE COMPRESSIBLE FLOW OVER AN AIRFOIL WITH A JET FLAP.IVES DC; MELNIK RE.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 7TH FLUID PLASMA DYN. CONF.; PALO ALTO, CALIF.; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 542; PP. 1-14; BIBL. 14 REF.Conference Paper

RELAXATION TECHNIQUES FOR THREE DIMENSIONAL TRANSONIC FLOW ABOUT WINGSBAILEY FR; STEGER JL.1973; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1973; VOL. 11; NO 3; PP. 318-325; BIBL. 17 REF.Serial Issue

A DIRECT METHOD FOR COMPUTING THE STEADY FLOW AT MACH NUMBER ONE PAST A GIVEN WING AIRFOILEUVRARD D; TOURNEMINE G.1973; LECTURE NOTES PHYS.; GERM.; DA. 1973; NO 19; PP. 146-152; BIBL. 8 REF.; (PROC. 3RD. INT. CONF. NUMER. METHODS FLUID MECH. II. PROBL. FLUID MECH.; PARIS; 1972)Conference Paper

TIME DEPENDENT CALCULATIONS FOR TRANSONIC FLOWBURSTEIN SZ; MIRIN AA.1973; LECTURE NOTES PHYS.; GERM.; DA. 1973; NO 19; PP. 48-59; BIBL. 10 REF.; (PROC. 3RD. INT. CONF. NUMER. METHODS FLUID MECH. II. PROBL. FLUID MECH.; PARIS; 1972)Conference Paper

A FINITE DIFFERENCE METHOD FOR THE SOLUTION OF THE TRANSONIC FLOW AROUND HARMONICALLY OSCILLATING WINGS.EHLERS FE.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 7TH FLUID PLASMA DYN. CONF.; PALO ALTO, CALIF.; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 543; PP. 1-6; BIBL. 15 REF.Conference Paper

INVERSE METHOD OF DESIGNING TWO-DIMENSIONAL TRANSONIC AIRFOIL SECTIONSSATO J.1973; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1973; VOL. 11; NO 1; PP. 58-63; BIBL. 29 REF.Serial Issue

NUMERICAL APPROACH FOR INVESTIGATING SOME TRANSONIC FLOWSBELOTSERKOVSKII OM; DAVIDOV YM.1973; LECTURE NOTES PHYS.; GERM.; DA. 1973; NO 19; PP. 25-32; BIBL. 12 REF.; (PROC. 3RD. INT. CONF. NUMER.METHODS FLUID MECH. II. PROBL. FLUID MECH.; PARIS; 1972)Conference Paper

APPROXIMATE SHOCK-FREE TRANSONIC SOLUTION FOR A SYMMETRIC PROFILE AT ZERO INCIDENCENIYOGI P; MITRA R.1973; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1973; VOL. 11; NO 5; PP. 751-754; BIBL. 7 REF.Serial Issue

THE CALCULATION OF SUBSONIC AND TRANSONIC TURBULENT BOUNDARY LAYERS ON AN INFINITE YAWED AIRFOIL.ADAMS JC JR.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 7TH FLUID PLASMA DYN. CONF.; PALO ALTO, CALIF.; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 557; PP. 1-18; BIBL. 2 P.Conference Paper

TRANSONIC FLOW PAST LIFTING WINGSNORSTRUD H.1973; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1973; VOL. 11; NO 5; PP. 754-757; BIBL. 7 REF.Serial Issue

NUMERICAL SIMULATION OF HIGH REYNOLDS NUMBER TRANSONIC FLOWS.DEIWERT GS.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 7TH FLUID PLASMA DYN. CONF.; PALO ALTO, CALIF.; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 603; PP. 1-6; BIBL. 3 REF.Conference Paper