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

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

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

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

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

COMPUTER INTERACTIVE GRAPHICS IN AEROSPACE ENGINEERING DESIGN EDUCATION.SMITH HW.1976; IN: AIRCR. SYST. TECHNOL. MEET. AM. INST. AERONAUT. ASTRONAUT.; DALLAS, TEX.; 1976; NEW YORK; AIAA; DA. 1976; PP. 1-11; BIBL. 12 REF.Conference Paper

COST ANALYSIS AS APPLIED TO AIRCRAFT SYNTHESIS = ANALYSE DU COUT APPLIQUEE A LA SYNTHESE DES AVIONSFISHER JF; HITCHCOCK ST; TRELEASE RH et al.sdIN: SOC. AERONAUT. WEIGHT ENG. INC. 31ST ANNU. CONF. ATLANTA, 1972; LOS ANGELES; S.A.W.E.; DA. S.D.; VOL. 913; PP. 1-25; BIBL. 5 REF.Conference Paper

AN APPROACH TO SYSTEM COST OPTIMIZATION = APPROCHE D'UN SYSTEME D'OPTIMISATION DU COUTGUINN SL.sdIN: SOC. AERONAUT. WEIGHT ENG. INC. 31ST ANNU. CONF. ATLANTA, 1972; LOS ANGELES; S.A.W.E.; DA. S.D.; VOL. 941; PP. (48 P.)Conference Paper

La dynamique institutionnelle à l'origine d'un nouveau mode d'insertion «locale» : le cas des relations entre Aérospatiale et ses sous-traitantsTALBOT, D.1998, 22 p.Book

MATERIAL DESIGN CONCEPTS FOR FILAMENT-WOUND, GRAPHITE-GRAPHITE HEATSHIELDS: FURTHER ANALYSIS = CONCEPTION DE MATERIAUX POUR BOUCLIERS THERMIQUES GRAPHITE-GRAPHITE A BOBINAGE DE FILAMENTS: ANALYSE SUPPLEMENTAIREGUESS TR; BERT CW.1973; J. SPACECR. ROCK.; U.S.A.; DA. 1973; VOL. 10; NO 2; PP. 159-160; BIBL. 3 REF.Serial Issue

A MIXED OPTIMIZATION METHOD FOR AUTOMATED DESIGN OF FUSELAGE STRUCTURES = UNE METHODE MIXTE D'OPTIMISATION POUR LA CONCEPTION AUTOMATIQUE DE STRUCTURES DE FUSELAGESOBIESZCZANSKI J; LOENDORF D.1972; J. AIRCR.; U.S.A.; DA. 1972; VOL. 9; NO 12; PP. 805-811; BIBL. 16 REF.Serial 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

LES ALLIAGES DANS LA CONSTRUCTION AEROSPATIALE DE DEMAINSTAMBLER I.1973; INTERAVIA; SUISSE; DA. 1973; VOL. 28; NO 4; PP. 349-351Serial Issue

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

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

INTERACTIVE 3D SHAPE DESIGN. MULTIPATCH AND MULTIOBJECT = CREATION CONVERSATIONNELLE DE FORMES EN 3 DIMENSIONS. MULTI-MORCEAU ET MULTI-OBJETARMIT AP.1973; AIRCR. ENGNG; G.B.; DA. 1973; VOL. 45; NO 2; PP. 13-17; BIBL. 4 REF.Serial Issue

THE DESIGN AND APPLICATION OF THE TRAVERSING INFRA-RED INSPECTION SYSTEM-TIRISCOHEN SE.1973; NON-DESTRUCT. TESTG; G.B.; DA. 1973; VOL. 6; NO 2; PP. 74-80; BIBL. 11 REF.Serial Issue

GOVERNMENT ASSISTANCE FOR TECHNICAL INFORMATION IN INDUSTRY AND SIMPLE MECHANIZATION FOR SMALL INFORMATION CENTRES. 25 TH. MEETING OF THE AGARD TECHNICAL INFORMATION PANEL. ANKARA, TURKEY, 23-24 OCTOBER 19721973; A.G.A.R.D. CONF. PROC.; FR.; DA. 1973; NO 117; PP. (99 P.); BIBL. DISSEM.Conference Paper

ADVANCED MATERIALS FOR AIRCRAFT BRAKESWEAVER JV.1973; TECH AIR; G.B.; DA. 1973; VOL. 29; NO 5; PP. 2-4Serial Issue