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A ROTARY ENGINE DEVELOPMENT.HUBBARD G.1976; A.I.A.A. MONOGR.; U.S.A.; DA. 1976; VOL. 21; PP. 47-48Article

ANTONIO FERRI. SELECTED PAPERS ON ADVANCED DESIGN OF AIR VEHICLES.1977; AGARD-AG-226; FR.; DA. 1977; PP. (138P.); BIBL. 11 P.; ISBN 9283512537Report

12C-12C TOTAL AND REACTION CROSS-SECTION BETWEEN 6 AND 85 MEV/A FROM AN OPTICAL MODEL ANALYSIS = SECTION EFFICACE TOTALE ET DE REACTION 12C-12C ENTRE 6 ET 85 MEV/A A PARTIR D'UNE ANALYSE PAR LE MODELE OPTIQUEBRANDAN ME.1982; ; FRA; DA. 1982; ISN/82-35; 13 P.-4 PL.; 30 CM; BIBL. 1 P.Report

K RACIONALIZACI PROCESU PROJEKTOVDNI A VYSTAVBY ASR = LA RATIONALISATION DU PROCEDE DE CONCEPTION ET DE CONSTRUCTION DES SYSTEMES DE COMMANDE AUTOMATIQUEPITRA Z.1980; AUTOMATIZACE; CSK; DA. 1980; VOL. 23; NO 6; PP. 157-161; BIBL. 8 REF.Article

A POTENTIAL FLOW DESIGN METHOD FOR MULTICOMPONENT AIRFOIL SECTIONS.KENNEDY JL; MARSDEN DJ.1978; J. AIRCR.; U.S.A.; DA. 1978; VOL. 15; NO 1; PP. 47-52; BIBL. 8 REF.Article

DESING OF TWO-DIMENSIONAL WIND TUNNEL CONTRACTIONS.MOREL T.1977; J. FLUIDS ENGNG; U.S.A.; DA. 1977; VOL. 99; NO 2; PP. 371-378; BIBL. 22 REF.Article

DEVELOPMENT OF A VERY LARGE RADIAL VORTEX VALVE.BROMBACH H; NEUMAYER H.1977; FLUIDICS QUART.; U.S.A.; DA. 1977; VOL. 9; NO 2; PP. 59-75; BIBL. 11 REF.Article

AN INITIAL APPROACH TO THE DESIGN OF VERY WIDE ANGLE AXISYMMETRIC DIFFUSERS WITH GAUZES TO ACHIEVE UNIFORM OUTLET VELOCITY PROFILES.KACHHARA NL; LIVESEY JL; WOLCOX PL et al.1977; J. FLUIDS ENGNG; U.S.A.; DA. 1977; VOL. 99; NO 2; PP. 357-374; BIBL. 11 REF.Article

DESIGN AND ANALYSIS OF A SPACE SEXTANT FOR HIGH ALTITUDE NAVIGATION.GARCIA HA; OWEN WJ.1976; J. SPACECR. ROCK.; U.S.A.; DA. 1976; VOL. 13; NO 12; PP. 705-711; BIBL. 6 REF.Article

TURBINE TEST CASES. PRESENTATION OF DESIGN AND EXPERIMENTAL CHARACTERISTICS.CHAUVIN J; SIEVERDING C.1976; A.G.A.R.D. CONF. PROC.; FR.; DA. 1976; NO 195; PP. 12.1-12.19; (THROUGH-FLOW CALC. AXIAL TURBOMACH. MEET. AGARD PROPUL. ENERG. PANEL. 47; PORZ-WAHN-KOELN; 1976)Conference Paper

CALCUL DU REGIME D'UNE SURFACE DE CONTACT "COUSUE" DANS UN TUBE DE CHOCPETROV RL.1976; INZHENER.-FIZ. ZH., BELORUS. S.S.R.; S.S.S.R.; DA. 1976; VOL. 31; NO 3; PP. 537-542; ABS. ANGL.; BIBL. 7 REF.Article

UTILISATION DES CRITERES DE SIMILITUDE DANS L'ETUDE D'UN PROJET DE TURBINES A VAPEURVESTEMEANU N.1976; NOUTATI MEC. APL. CONTR. MASINI, A; ROMAN.; DA. 1976; VOL. 18; PP. 115-120; ABS. FR.; BIBL. 3 REF.Article

A STRAIGHT FORWARD AND FLEXIBLE DESIGN METHOD FOR COMPLEX DATA BASE MANAGEMENT SYSTEMSJONKERS HL.1973; INFORM. STORAGE RETRIEV.; G.B.; DA. 1973; VOL. 9; NO 7; PP. 401-415; BIBL. 12REF.Serial Issue

ETUDE EXPERIMENTALE DES PROPRIETES DES EVENEMENTS DIMUONS DE MEME SIGNE ET DES EVENEMENTS TRIMUONS DANS LES INTERACTIONS DE NEUTRINOS ET D'ANTINEUTRINOS A HAUTE ENERGIE = EXPERIMENTAL STUDY OF PROPERTIES OF DIMUON EVENTS WITH SAME SIGNS AND TRIMUON EVENTS IN NEUTRINO AND ANTINEUTRINO INTERACTIONS AT HIGH ENERGYPEYAUD BERNARD.1983; ; FRA; DA. 1983; CEA-N/2324; 104 P.-57 PL.; 30 CM; BIBL. 50 REF.Report

AN UNDERGRADUATE DESIGN. PROJECT COURSE UTILIZING A MICROCOMPUTERGAULT JW; SNYDER WE.1978; I.E.E.E. TRANS. EDUC.; USA; DA. 1978; VOL. 21; NO 4; PP. 240-243; BIBL. 5 REF.Article

COMPUTERS AND WIND TUNNELS. COMPLEMENTARY AIDS TO AIRCRAFT DESIGN.HAINES AB.1977; AERONAUT. J.; G.B.; DA. 1977; VOL. 81; NO 799; PP. 306-321; BIBL. 48 REF.Article

BEITRAG ZUR BERECHNUNG VON KENNFELDERN MEHRSTUFIGER AXIALVERDICHTER. = CONTRIBUTION AU CALCUL DES PERFORMANCES DES COMPRESSEURS AXIAUX A PLUSIEURS ETAGESGRAHL KG.1977; Z. FLUGWISSENSCH. WELTR.-FORSCH.; DTSCH.; DA. 1977; VOL. 1; NO 2; PP. 116-122; ABS. ANGL.; BIBL. 5 REF.Article

A GENERAL ROTOR MODEL SYSTEM FOR WIND-TUNNEL INVESTIGATIONS.WILSON JC.1977; J. AIRCR.; U.S.A.; DA. 1977; VOL. 14; NO 7; PP. 639-643; BIBL. 8 REF.Article

TRENDS IN THE DESIGN OF FUTURE COMMUNICATIONS SATELLITE SYSTEMSHARTL H; BARTBAUM H; TREYTL H et al.1981; ACTA ASTRONAUT.; ISSN 0094-5765; USA; DA. 1981; VOL. 8; NO 2; PP. 209-223; BIBL. 13 REF.Article

RAPPORT ANNUEL. 1981 = ANNUAL REPORT. 19811981; ; FRA; GRENOBLE: IN2P3, INSTITUT DES SCIENCES NUCLEAIRES DE GRENOBLE; DA. 1981; ISN/82-18; 110 P.; 30 CMReport

THE INDIRECT DESIGN OF FLUID CHANNELS USING A GLOBAL VARIATIONAL METHOD WITH TRIAL FUNCTIONS NOT SATISFYING THE PRESCRIBED BOUNDARY CONDITIONS. II. COUPLING METHOD.HENDRY JA.1978; INTERNATION. J. NUMER. METHODS ENGNG; G.B.; DA. 1978; VOL. 12; NO 3; PP. 471-477; BIBL. 11 REF.Article

ANALYSIS OF A PISTON-DRIVEN SHOCK TUBE.BEN DOR G; IGRA O.1978; AERONAUT. J.; G.B.; DA. 1978; VOL. 82; NO 808; PP. 178-181; BIBL. 5 REF.Article

COMPUTER UND WINDKANAELE: ERGAENZENDE HILFEN FUER DEN FLUGZEUGENTWURF. = L'ORDINATEUR ET LES SOUFFLERIES, DES AUXILIAIRES COMPLEMENTAIRES POUR LA CONCEPTION DES AVIONSHAINES AB.1977; Z. FLUGWISSENSCH. WELTR.-FORSCH.; DTSCH.; DA. 1977; VOL. 1; NO 5; PP. 321-337; ABS. ANGL.; BIBL. 48 REF.Article

SIMULATION STATISTIQUE DE LA MISE AU POINT OPTIMALE DES PARAMETRES D'UNE TURBINE A GAZMELUZOV YU V.1977; IZVEST. VYSSH. UCHEBN. ZAVED., AVIAC. TEKH.; S.S.S.R.; DA. 1977; VOL. 20; NO 1; PP. 83-88; BIBL. 5 REF.Article

GRUNDASPEKTE DER BEWERTUNG UND GESTALTUNG VON DOKUMENTATIONS -UND INFORMATIONSSYSTEMEN = ASPECTS FONDAMENTAUX DE L'EVALUATION ET DE L'ORGANISATION DE SYSTEMES DOCUMENTAIRES1972; NACHR. DOKUMENT.; DTSCH.; DA. 1972; VOL. 23; NO 5; PP. 194-202; ABS. ANGL.; BIBL. 15REF.Serial Issue

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