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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

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

SOME TUNNEL-WALL EFFECTS ON TRANSONIC FLUTTER.RUHLIN CL; DESTUYNDER RM; GREGORY RA et al.1975; J. AIRCR.; U.S.A.; DA. 1975; VOL. 12; NO 3; PP. 162-167; BIBL. 10 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

EXPERIMENTAL INVESTIGATION OF A TRANSONIC AXIAL FLOW COMPRESSOR STAGE WITH STEADY STATE DISTORTED INLET FLOW.LECHT M; WEYER H.sdIN: 2ND INT. SYMP. AIR BREATHING ENGINES. PROC.; SHEFFIELD, ENGL.; 1974; LONDON; R. AERONAUT. SOC.; DA. S.D.; PP. (15P.); BIBL. 4 REF.Conference Paper

TRACE DES AUBAGES DE TURBINE TRANSSONIQUES PAR LA METHODE DE L'HODOGRAPHE.KARADIMAS G.sdIN: 2ND INT. SYMP. AIR BREATHING ENGINES. PROC.; SHEFFIELD, ENGL.; 1974; LONDON; R. AERONAUT. SOC.; DA. S.D.; PP. (15P.); BIBL. 8 REF.Conference Paper

A NOTE ON TRANSONIC FLOW PAST A THIN AVIFOIL OSCILLATING IN A WIND TUNNEL.SAVKAR SD.1976; J. SOUND VIBR.; G.B.; DA. 1976; VOL. 46; NO 2; PP. 195-207; BIBL. 16 REF.Article

EFFECTS OF REYNOLDS NUMBER ON SWEPT-WING-BODY CONFIGURATIONS WITH HIGH LIFT DEVICES AT TRANSONIC SPEEDS.ATRAGHJI E; SORENSEN H.1974; IN: 9TH CONGR. INT. COUNC. AERONAUT. SCI. PROC.; HAIFA; 1974; JERUSALEM; WEIZMANN SCI. PRESS ISR.; DA. 1974; VOL. 1; PP. 94-120; BIBL. 8 REF.Conference Paper

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

ETUDE DE L'ECOULEMENT DANS UN EJECTEUR TRANSSONIQUE.HARDY JM; DUTOUQUET L.1974; AERONAUT. ET ASTRONAUT.; FR.; DA. 1974; NO 47; PP. 62-69; ABS. ANGL. ALLEM.; BIBL. 10 REF.Article

MEASUREMENTS OF FLOW QUALITY IN THE AMES 2 X 2 FT TRANSONIC WIND TUNNELOWEN FK.1981; AEROSPACE SCIENCES MEETING. 19 /1981-01-12/SAINT LOUIS MO; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1981; 6 P.; BIBL. 2 REF.Conference Paper

THE DEVELOPMENT OF A SELF-STREAMLINING FLEXIBLE WALLED TRANSONIC TEST SECTIONGOODYER MJ; WOLF SWD.1980; AERODYNAMICS TESTING CONFERENCE. 11/1980/COLORADO SPRINGS CO; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1980; PP. 325-335; BIBL. 9 REF.Conference Paper

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

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

TRANSONIC WALL INTERFERENCE EFFECTS ON BODIES OF REVOLUTIONCOUCH LM.sdIN: AIAA 7TH AERODYN. TEST. CONF. PALO ALTO, CALIF., 1972; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. S.D.; NO 993; PP. 1-5; BIBL. 4 REF.Conference Paper

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

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

IL-22 : A critical mediator in mucosal host defenseAUJLA, S. J; KOLLS, J. K.Journal of molecular medicine (Berlin. Print). 2009, Vol 87, Num 5, pp 451-454, issn 0946-2716, 4 p.Article

CONVERGENCE TO UNCONFINED FLOW OF THE THREE-DIMENSIONAL TRANSONIC SELF-CORRECTING WIND TUNNELSHU CHIEH WANG.1981; COMPUT. METHODS APPL. MECH. ENG.; ISSN 0045-7825; NLD; DA. 1981; VOL. 28; NO 2; PP. 191-205; BIBL. 5 REF.Article

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