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PROBLEME DE L'OPTIMISATION DES PARAMETRES D'UN AVIONGOGOLIN VP; NIKITIN AI.1972; IZVEST. VYSSH. UCHEBN. ZAVED., AVIAC. TEKH.; S.S.S.R.; DA. 1972; NO 4; PP. 126-129; BIBL. 4 REF.Serial Issue

PROGRAMMES D'ENTRETIEN MODERNES POUR AVIONS DE TRANSPORTMATTESON TD.1973; AERONAUT. ET ASTRONAUT.; FR.; DA. 1973; NO 40; PP. 24-29; ABS. ANGL. ALLEMSerial Issue

VORTEX MEASUREMENTS BEHIND A SWEPT WING TRANSPORT MODEL.ORLOFF KL; CIFFONE DL.1974; J. AIRCR.; U.S.A.; DA. 1974; VOL. 11; NO 6; PP. 362-364; BIBL. 8 REF.Article

THE GTCP331 AUXILIARY POWER UNIT FOR THE NEET GENERATION COMMERCIAL TRANSPORTSWELLS RE; ROMANIN AL.1980; SAE TRANS.; ISSN 0096-736X; USA; DA. 1980; VOL. 89; NO 4; PP. 3479-3495Article

ADVANCED OLYMPUS FOR NEXT GENERATION SUPERSONIC TRANSPORT AIRCRAFTGUPTA PC.1980; SAE TRANS.; ISSN 0096-736X; USA; DA. 1980; NO 2; PP. 2265-2289; BIBL. 20 REF.Article

INSONORISATION D'UN HALL DE REPARATION DE BOEING AIR FRANCE, ORLY1981; TECH. MOD.; ISSN 0040-1250; FRA; DA. 1981; VOL. 73; NO 5-6; PP. 77-78Article

SIFT: DESIGN AND ANALYSIS OF A FAULT-TOLERANT COMPUTER FOR AIRCRAFT CONTROL = SIFT: CONCEPTION ET ANALYSE D'UN CALCULATEUR TOLERANT AUX FAUTES POUR LA COMMANDE D'AVIONSWENSLEY JH; LAMPORT L; GOLDBERG J et al.1978; PROC. I.E.E.E.; USA; DA. 1978; VOL. 66; NO 10; PP. 1240-1255; BIBL. 12 REF.Article

OPTIMISME CIRCONSPECT AU SEIN D'AIRBUS INDUSTRIE1973; INTERAVIA; SUISSE; DA. 1973; VOL. 28; NO 4; PP. 356Serial Issue

THE UNITED STATES SST AND AIR QUALITYSWIHART JM.1971; S.A.E. TRANS.; U.S.A.; DA. 1971; VOL. 80; PART 2; PP. 1344-1354; BIBL. 19 REF.Serial Issue

ATLANTA AIRPORT TERMINAL COMPLEX = LE COMPLEXE DU TERMINAL DE L'AEROPORT D'ATLANTA1981; CIV. ENG. ASCE; ISSN 0360-0556; USA; DA. 1981; VOL. 51; NO 6; PP. 50-52Article

PROPFAN PROPULSION FOR COMMERCIAL AIR TRANSPORTSCOUSSENS TG; TULLIS RH.1980; SAE TRANS.; ISSN 0096-736X; USA; DA. 1980; NO 2; PP. 2290-2296; BIBL. 3 REF.Article

POWERPLANT INTEGRATION - THE APPLICATION OF CURRENT EXPERIENCE TO FUTURE DEVELOPMENTSBROWN TW; TALBOT JE.1979; J. ENG. POWER; ISSN 0022-0825; USA; DA. 1979; VOL. 101; NO 2; PP. 259-269; BIBL. 8 REF.Article

CRITERE D'EVALUATION DE L'EFFICACITE DE L'EQUIPEMENT DES SYSTEMES ELECTROENERGETIQUES DES MOYENS DE TRANSPORTKRIVENTSEV VI.1978; IZVEST. AKAD. NAUK S.S.S.R., ENERGET. TRANSP.; S.S.S.R.; DA. 1978; NO 1; PP. 36-43; BIBL. 4 REF.Article

FIMP - A HIGHLY RELIABLE FAULT-TOLERANT MULTIPROCESSOR FOR AIRCRAFT = MPTF: MULTIPROCESSEUR TOLERANT AUX FAUTES TRES FIABLE POUR LES AVIONSHOPKINS AL JR; SMITH TB III; LALA JH et al.1978; PROC. I.E.E.E.; USA; DA. 1978; VOL. 66; NO 10; PP. 1221-1239; BIBL. 19 REF.Article

PREDICTION METHODS FOR AIRCRAFT AERODYNAMIC CHARACTERISTICS.1974; AGARD-LS-67; FR.; DA. 1974; PP. (349P.); BIBL. DISSEM.Report

A SIMPLIFIED ALTERNATIVE TO CURRENT AIRLINE FUEL ALLOCATION MODELSNASH B.1981; INTERFACES (BALTIMORE, MD.); ISSN 0092-2102; USA; DA. 1981; VOL. 11; NO 1; PP. 1-8Article

ELECTRICAL POWER-FACTORS TO BE CONSIDERED IN FUTURE CIVIL AIRCRAFT OF MODERATE COMPLEXITY.DHURY HP.1977; AERONAUT. J.; G.B.; DA. 1977; VOL. 81; NO 803; PP. 502-508; BIBL. 1 REF.Article

THE CRYSTAL BALL FOCUSES ON THE NEXT GENERATION OF TRANSPORT AIRCRAFTBLACK RE; MURPHY CG; STERN JA et al.1971; S.A.E. TRANS.; U.S.A.; DA. 1971; VOL. 80; NO PART 4; PP. 2485-2496Serial Issue

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