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

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

NDT IN THE AEROSPACE INDUSTRY. THE STATE OF THE ART. ULTRASONICSBUNCE HG.1973; BRIT. J. NON-DESTRUCT. TESTG; G.B.; DA. 1973; VOL. 15; NO 2; PP. 55-57Serial Issue

REVISED CALCULATIONS OF THE NACA 6-SERIES OF LOW DRAG AEROFOILS = CALCUL REVISE DE PROFILS A FAIBLE TRAINEE DE LA SERIE NACA-6NONWEILER TRF.1973; AERONAUT. J.; G.B.; DA. 1973; VOL. 77; NO 748; PP. 190-192; BIBL. 2 REF.Serial Issue

PARIS. LE BOURGET 19731973; INTERAVIA; SUISSE; DA. 1973; VOL. 28; NO 8; PP. 834-843Serial 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

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

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

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

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

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

BALLISTICS.1977; IN: ICIASF' 77. INT. CONGR. INSTRUM. AEROSP. SIMULATION FACIL. REC.; SHRIVENHAM, ENGL.; 1977; NEW YORK; INST. ELECTR. ELECTRON. ENG.; DA. 1977; PP. 135-194; BIBL. DISSEM.Conference Paper

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

AUTOMATED PROCEDURES FOR SIZING AEROSPACE VEHICLE STRUCTURES. (SAVES) = PROCEDURES AUTOMATIQUES DE CALCUL DE STRUCTURES DE VEHICULES AEROSPATIAUX (SAVES)GILES GL; BLACKBURN CL; DIXON SC et al.1972; J. AIRCR.; U.S.A.; DA. 1972; VOL. 9; NO 12; PP. 812-819; BIBL. 25 REF.Serial Issue

MISSION "SPACELAB" A EXAMEN O.R.L.BLANC P.1978; MED. AERONAUT. SPATIALE MED. SUBAQUAT. HYPERBARE; FRA; DA. 1978; VOL. 17; NO 66; PP. 12-13Article

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

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

NUMERICAL STUDY OF NON-UNIFORM AXISYMMETRIC UNDER-EXPANDED SUPERSONIC JET IMPINGEMENT ON A FINITE DISC.SANKARA RAO K; PUROHIT SC; SARMA MS et al.1976; AERONAUT. J.; G.B.; DA. 1976; VOL. 80; NO 787; PP. 313-317; BIBL. 5 REF.Article

SAFETY AND THE AMERICAN SPACE PROGRAM = LA SECURITE ET LE PROGRAMME SPATIAL AMERICAINTHORNTON WE.1974; AEROSPACE MED.; U.S.A.; DA. 1974; VOL. 45; NO 8 SECT. 2; PP. 924-927; (JT. COMM. AVIAT. PATHOL. 8TH. SCI. SESS.; COLORADO SPRINGS; COLO.; 1972)Conference Paper

THE ROLE OF THE PROJECT MANAGER IN THE MANAGEMENT OF SATELLITE PROJECTS = LE ROLE DU RESPONSABLE DE PROJET DANS L'ORGANISATION DE PROJETS DE SATELLITESCONCHIE PJ.1973; J. BRIT. INTERPLANET. SOC.; G.B.; DA. 1973; VOL. 26; NO 4; PP. 242-245; BIBL. 2 REF.Serial Issue

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