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AKUSTISCHE MESSUNG DER ZIRKULATION VON WIRBELN UND VON ZIRKULATIONSVERTEILUNGEN BEI MODELLUNTERSUCHUNGEN IN WINDKANAELEN. = MESURE ACOUSTIQUE DE LA CIRCULATION DES TOURBILLONS ET DE LA DISTRIBUTION DE CIRCULATION DANS DES ESSAIS SUR MAQUETTE EN SOUFFLERIESCHMIDT DW.1975; MITT. MAX-PLANCK-INST. STROEMUNGSFORSCH. AERODYN. VERSUCHSANST.; DTSCH.; DA. 1975; NO 6; PP. 1-95; H.T. 2; BIBL. 1 P.Serial Issue

MEASUREMENT OF TEMPERATURE IN FAST FLOWING AIR STREAMS. A GOLD FILM PROBE OF HIGH SENSITIVITY.SCHMIDT DW.1974; GOLD BULL.; S. AFR.; DA. 1974; VOL. 7; NO 4; PP. 103; BIBL. 2 REF.Article

IMMUNOGENICITY AND ANTIGENICITY OF HUMAN CORONAVIRUSES 229E AND OC43SCHMIDT DW; KENNY GE.1981; INFECT. IMMUN.; ISSN 0019-9567; USA; DA. 1981; VOL. 32; NO 3; PP. 1000-1006; BIBL. 28 REF.Article

COMPUTER-CONTROLLED STRESS INTENSITY GRADIENT TECHNIQUE FOR HIGH RATE FATIGUE CRACK GROWTH TESTING = TECHNIQUE DU GRADIENT D'INTENSITE DES CONTRAINTES CONTROLE INFORMATIQUEMENT POUR LES ESSAIS DE PROPAGATION DE FATIGUE A GRANDE VITESSEDONALD JK; SCHMIDT DW.1980; J. TEST. EVAL.; ISSN 0090-3973; USA; DA. 1980; VOL. 8; NO 1; PP. 19-24; BIBL. 5 REF.Article

FLOW OBSERVATIONS IN THE NEAR-WAKE OF CIRCULAR CYLINDERS BY MEASUREMENT OF THE TEMPERATURE FLUCTUATIONS.SCHMIDT DW; WAGNER WJ.1978; Z. FLUGWISSENSCH. WELTR.-FORSCH.; DTSCH.; DA. 1978; VOL. 2; NO 1; PP. 10-15; ABS. ALLEM.; BIBL. 8 REF.Article

UNTERSUCHUNG DES VON EINEM TRAGFLUEGELMODELL IM WINDKANAL ERZEUTEN WIRBELFELDES MITTELS ULTRASCHALLIMPULSEN = ETUDE DU CHAMP DE TOURBILLONS GENERE PAR UNE MAQUETTE DE PROFIL AERODYNAMIQUE DANS UNE SOUFFLERIE AU MOYEN DE PULSATIONS ULTRASONORESENGLER RH; SCHMIDT DW.1979; MITT. MAX-PLANCK-INST. STROEMUNGSFORSCH. AERODYN. VERSUCHSAMT.; DEU; DA. 1979; NO 69; PP. 1-149; ABS. ENG; BIBL. 12 REF.Serial Issue

EXPERIMENTS ON SECOND-SOUND SHOCK WAVES IN SUPERFLUID HELIUM.CUMMINGS JC; SCHMIDT DW; WAGNER WJ et al.1978; PHYS. OF FLUIDS; U.S.A.; DA. 1978; VOL. 21; NO 5; PP. 713-717; BIBL. 13 REF.Article

EXPERIMENTS ON THE CIRCULATION AND PROPAGATION OF LARGE-SCALE VORTEX RINGS IN HE IIBORNER H; SCHMELING T; SCHMIDT DW et al.1983; PHYSICS OF FLUIDS; ISSN 0031-9171; USA; DA. 1983; VOL. 26; NO 6; PP. 1410-1416; BIBL. 19 REF.Article

INTERACTION OF A VORTEX WITH A NON-LINEAR SHEAR FLOWALBERS F; SCHMIDT DW; WAGNER WJ et al.1980; AERONAUT. J.; GBR; DA. 1980; VOL. 84; NO 830; PP. 70-72; BIBL. 8 REF.Article

ULTRASONIC METHOD FOR FLOW FIELD MEASUREMENT IN WIND TUNNEL TESTSENGLER RH; SCHMIDT DW; WAGNER WJ et al.1982; J. ACOUST. SOC. AM.; ISSN 0001-4966; USA; DA. 1982; VOL. 71; NO 1; PP. 41-50; BIBL. 14 REF.Article

THE DEINSTITUTIONALIZED CITIZEN: ADJUSTMENT AND QUALITY OF LIFE.MCDEWITT SC; SMITH PM; SCHMIDT DW et al.1978; MENTAL RETARDAT.; U.S.A.; DA. 1978; VOL. 16; NO 1; PP. 22-24; BIBL. 1 REF.Article

COMPUTER-CONTROLLED DECREASING STRESS INTENSITY TECHNIQUE FOR LOW RATE FATIGUE CRACK GROWTH TESTING.SAXENA A; HUDAK SJ JR; DONALD JK et al.1978; J. TESTG EVAL.; USA; DA. 1978; VOL. 6; NO 3; PP. 167-174; BIBL. 10 REF.Article

TENTATIVE TEST PROCEDURE FOR DETERMINING THE PLANE STRAIN J1-R CURVE = PROJET DE METHODE D'ESSAI POUR DETERMINER LA COURBE J1-R EN DEFORMATION PLANEALBRECHT P; ANDREWS WR; GUDAS JP et al.1982; JOURNAL OF TESTING AND EVALUATION; ISSN 0090-3973; USA; DA. 1982; VOL. 10; NO 6; PP. 245-251; BIBL. 9 REF.Article

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