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

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

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

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

Welche Kältemittel in der Zukunft? = Which refrigerant in the future?DOÊRING, R.Die Kälte und Klimatechnik. 1990, Vol 43, Num 9, pp 472-482, issn 0343-2246, 6 p.Article

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

Th17 cytokines and mucosal immunityDUBIN, Patricia J; KOLLS, Jay K.Immunological reviews. 2008, Vol 226, pp 160-171, issn 0105-2896, 12 p.Article

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

Investigations of transonic Ludwieg tubes. III: Effects of plenum exhaust system on starting process of tunnel test sectionKAGE, K; MATSUO, K; KAWAGOE, S et al.Bulletin of the JSME. 1985, Vol 28, Num 243, pp 1868-1873, issn 0021-3764Article

IL-22, but Not IL-17, Dominant Environment in Cutaneous T-cell LymphomaMIYAGAKI, Tomomitsu; SUGAYA, Makoto; SUGA, Hiraku et al.Clinical cancer research (Print). 2011, Vol 17, Num 24, pp 7529-7538, issn 1078-0432, 10 p.Article

Installation avec évaporateur à air et condenseur à air = Refrigerating unit with an air evaporator and an air condenserJACQUARD, P.Revue pratique du froid et du conditionnement d'air. 1998, Num 862, pp 49-50, issn 0370-6699Article

Verwendung von KLEA 407A bei überfluteter Verdampfung = Using KLEA 407A with flooding evaporationLOW, B; TAYLOR, A.Die Kälte und Klimatechnik. 1996, Vol 49, Num 8, pp 528-531, issn 0343-2246, 3 p.Article

Austauschstoffe für R22: ein Überblick = Substitutes for R22: an overviewSCHWENNESEN, K.Die Kälte und Klimatechnik. 1994, Vol 47, Num 2, pp 59-62, issn 0343-2246, 3 p.Article

Do we understand the 22-year solar activity cycle ?PATERNO, L.Comptes rendus de l'Académie des sciences. Série IIb, mécanique, physique, astronomie. 1998, Vol 326, Num 6, pp 393-405, issn 1287-4620Article

Options techniques des constructeurs pour l'après-R 22 = Technical options for manufacturers about R 22 substituteMALEK, A; GOTH, Y.Revue pratique du froid et du conditionnement d'air. 1996, Num 833BIS, pp 49-53, issn 0370-6699Article

Le programme des R 407C et R 410B : Climatisation = R 407C and R 410B as substitutes of R 22 : Air conditioningDUBOIS, L; RINALDI, R.Revue pratique du froid et du conditionnement d'air. 1995, Num 818, pp 48-49, issn 0370-6699Article

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