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DIE WIRTSCHAFTLICHE VERWENDUNG VON BLECHEN IM FLUGZEUGBAU = L'UTILISATION ECONOMIQUE DES TOLES DANS LA FABRICATION DES AVIONS1973; INDUSTR.-ANZ.; DTSCH.; DA. 1973; VOL. 95; NO 10; PP. 168-170Serial Issue

IMPIEGO DELL'ALLUMINIO NEGLI AEREI MODERNI = EMPLOI DE L'ALUMINIUM DANS LES AVIONS MODERNES1972; ALLUMINIO; ITAL.; DA. 1972; VOL. 41; NO 11-12; PP. 595-598Serial Issue

GLI ELICOTTERI. 85 COMPONENTI SU 100 SONO DI ALLUMINIO = LES HELICOPTERES. 85 COMPOSANTS SUR 100 SONT EN ALUMINIUMMIANA C.1973; ALLUMINIO; ITAL.; DA. 1973; VOL. 42; NO 1; PP. 4-13Serial Issue

STRESSKIN ADDS TO PAYLOAD = LES STRUCTURES STRESSKIN PERMETTENT D'AUGMENTER LE POIDS UTILE1973; IRON AGE METALWORKG INTERNATION.; U.S.A.; DA. 1973; VOL. 12; NO 2; PP. 26; ABS. ALLEM. FR. ESPSerial Issue

L'AVIATION GENERALE EN FRANCE1973; INTERAVIA; SUISSE; DA. 1973; VOL. 28; NO 5; PP. 498-500Serial Issue

THE EARLY DETECTION OF FATIGUE DAMAGE BY EXOELECTRON EMISSION AND ACOUSTIC EMISSIONMOORE JF; TSANG S.1972; A.S.T.M. SPEC. TECH. PUBL.; U.S.A.; DA. 1972; NO 515; PP. 143-157; BIBL. 1 P.; (TEST. PREDICT. MATER. PERFORMANCE STRUCT. COMPONENTS. SYMP.; I. II. ANAHEIM, CALIF.-ATLANTIC CITY, N.J.; 1971)Conference Paper

LEISTUNGSERHOELUNG DURCH REGLERGESTUETZTEN FLUGZEUGENTWURF = ELEVATION DE LA PUISSANCE PAR L'INTRODUCTION DU CONTROLE DANS L'ETABLISSEMENT D'UN PROJET D'AVIONLOBERT G.sdIN: 5. JAHRESTAG. DTSCH. GES. LUFT RAUMFAHRT; BERLIN; 1972; S.L.; DA. S.D.; PP. 1-24; BIBL. 7 REF.Conference Paper

L'INDUSTRIE AEROSPATIALE AMERICAINE: SITUATION ACTUELLE ET PERSPECTIVES D'AVENIRGEDDES JP.1973; INTERAVIA; SUISSE; DA. 1973; VOL. 28; NO 5; PP. 518-524Serial Issue

L'AVIATION EN AUSTRALASIE. I. LA PRODUCTION AERONAUTIQUEMUIR N.1973; INTERAVIA; SUISSE; DA. 1973; VOL. 28; NO 3; PP. 254-256Serial Issue

SOCIETY OF AUTOMOTIVE ENGINEERS. NATIONAL AEROSPACE ENGINEERING AND MANUFACTURING MEETING. SAN DIEGO, CALIFORNIA, OCTOBER 2-5, 1972 = SOCIETY OF AUTOMOTIVE ENGINEERS. MEETING NATIONAL SUR LE GENIE AEROSPATIAL. SAN DIEGO, CALIFORNIA, 2-5 OCTOBRE 19721972; NEW YORK; SOC. AUTOMOT. ENG.; DA. 1972; PP. (561 P.); H.T. 46; BIBL. DISSEM.; 56 FASCConference Paper

A GUIDE TO FASTENERS FOR USE AT ELEVATED TEMPERATURES1973; MATER. ENGNG; U.S.A.; DA. 1973; VOL. 77; NO 2; PP. 69-70Serial Issue

MATERIALS FIGHT HEAT IN AIRCRAFT JET ENGINESVACCARI JA.1973; MATER. ENGNG; U.S.A.; DA. 1973; VOL. 77; NO 2; PP. 19-22Serial Issue

OPTIMISATION IN CONSTRUCTION OF THE JAGUAR AND OTHER MILITARY AIRCRAFTTAIG IC; KERR RI.1973; AIRCR. ENGNG; G.B.; DA. 1973; VOL. 45; NO 1; PP. 9-11; BIBL. 6 REF.Serial Issue

DESIGN PARAMETERS FOR TORSION OF SANDWICH STRIPS HAVING TRAPEZOIDAL, RECTANGULAR, AND TRIANGULAR CROSS SECTIONSMONTREY HM; KUENZI EW.1972; U.S.D.A. FOREST SERV. RES. PAPER; U.S.A.; DA. 1972; NO 156; PP. (39 P.); BIBL. 6 REF.Serial Issue

LE CHOIX DES MATERIAUX UTILISES SUR CONCORDESERTOUR G; HILAIRE G; BEZAUD C et al.1973; METALLURG. CONSTR. MEC.; FR.; DA. 1973; VOL. 105; NO 1-2; PP. 3-15Serial Issue

LE NORSIAL, MATERIAU D'AVENIR DANS LES TECHNIQUES AEROSPATIALESSPINCOURT J.1973; INTERAVIA; SUISSE; DA. 1973; VOL. 28; NO 4; PP. 352Serial Issue

ADHESIVE BONDING OF HIGH MODULUS COMPOSITE AIRCRAFT STRUCTURESDASTIN SJ; LUBIN G.1971; S.A.E. TRANS.; U.S.A.; DA. 1971; VOL. 80, PART. 1; PP. 379-384Serial Issue

BOEING A VENDU UN MILLIER DE 727 ET ESPERE EN VENDRE ENCORE BEAUCOUPGEDDES JP.1973; INTERAVIA; SUISSE; DA. 1973; VOL. 28; NO 3; PP. 245-247Serial Issue

CONCORDE: UN NOUVEL ECUEIL DANS UNE PASSE DIFFICILEDURON M; DEFAUX M.1973; MACH. MOD.; FR.; DA. 1973; NO 768; PP. 4-6Serial Issue

LE SALON DE READING 1973HOLLAHAN J.1973; INTERAVIA; SUISSE; DA. 1973; VOL. 28; NO 8; PP. 844-846Serial Issue

COMPRESSIVE STRENGTH OF TITANIUM ALLOY SKIN-STRINGER PANELS SELECTIVITY REINFORCED WITH BORON-ALUMINIUM COMPOSITE = RESISTANCE A LA COMPRESSION DE PANNEAUX EN ALLIAGE DE TITANE RENFORCES DE FACON SELECTIVE PAR UN COMPOSITE BORE-ALUMINIUMHERRING HW; CARRI RL.1972; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1972; VOL. 10; NO 12; PP. 1555-1556; BIBL. 3 REF.Serial Issue

SURVEY OF COMPUTER-ASSISTED WRITING AND EDITING SYSTEMS.BERMAN PI.1977; AGARD-AG-229; FR.; DA. 1977; PP. 1-58; BIBL. 1 P. 1/2; ISBN 9283512510Report

DEVELOPMENT OF A PHASE CHANGE THERMAL CONTROL DEVICE = MISE AU POINT D'UN DISPOSITIF DE CONTROLE THERMIQUE A CHANGEMENT DE PHASESCHELDEN BG; GOLDEN JO.1973; J. SPACECR. ROCK.; U.S.A.; DA. 1973; VOL. 10; NO 2; PP. 99-100; BIBL. 4 REF.Serial Issue

FLUGZEUGLACKIERUNG UND FARBSPRITZANLAGEN = PEINTURES D'AVION ET INSTALLATIONS DE PULVERISATION AU PISTOLETGLISSMANN H.1973; INDUSTR.-LACKIER-BETRIEB; DTSCH.; DA. 1973; VOL. 41; NO 2; PP. 55-57Serial Issue

COMPARAISON DES METHODES DE MISE AU POINT EN EUROPE ET AUX ETATS-UNISPERRY R.1973; INTERAVIA; SUISSE; DA. 1973; VOL. 28; NO 4; PP. 322-324Serial Issue

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