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

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

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

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

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

HELICOPTER ROTOR BLADESPINCKNEY RL.1973; A.S.T.M. SPEC. TECH. PUBL.; U.S.A.; DA. 1973; NO 524; PP. 108-133; BIBL. 7 REF.Serial Issue

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

MILITARY AIRCRAFTHACKMAN LE.1973; A.S.T.M. SPEC. TECH. PUBL.; U.S.A.; DA. 1973; NO 524; PP. 43-75; BIBL. 21 REF.Serial Issue

FLIGHT EVALUATION OF A QUARTZ-FIBERFRAX HEAT SHIELD = EVALUATION EN VOL D'UN BOUCLIER THERMIQUE EN QUARTZ-FIBERFRAXGREENWALD GF.1972; J. SPACECR. ROCK.; U.S.A.; DA. 1972; VOL. 9; NO 12; PP. 939-940; BIBL. 2 REF.Serial Issue

A REVIEW OF THERMAL CONTROL MATERIALS FOR METALLIC JUNCTIONS = UN PASSAGE EN REVUE DE MATERIAUX DE CONTROLE THERMIQUE POUR DES JONCTIONS METALLIQUESFLETCHER LS.1972; J. SPACECR. ROCK.; U.S.A.; DA. 1972; VOL. 9; NO 12; PP. 849-850; BIBL. 7 REF.Serial Issue

MATERIAUX COURAMMENT EMPLOYES DANS LES PIECES A HAUTE TEMPERATURE DES TURBINES A GAZ AERONAUTIQUESBRUNETAUD M.1973; A.G.A.R.D. CONF. PROC.; FR.; DA. 1973; NO 120; PP. 31-42; ABS. ANGL; (ADVIS. GROUP. AEROSP. RES. DEV. CONF. PROC. HIGH TEMP. CORROS. AEROSP. ALLOYS; LYNGBY; 1972)Conference Paper

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

ACHIEVING FAIL SAFE DESIGN IN ROTORS = REALISATION DE LA SECURITE A LA DEFAILLANCE DES ROTORSFIELD DM; FINNEY RH; STRATTON WK et al.1973; J. AMER. HELICOPTER SOC.; U.S.A.; DA. 1973; VOL. 18; NO 1; PP. 29-35; BIBL. 3 REF.Serial Issue

COMMERCIAL AIRCRAFTJUNE RR; LAGER JR.1973; A.S.T.M. SPEC. TECH. PUBL.; U.S.A.; DA. 1973; NO 524; PP. 1-42; BIBL. 5 REF.Serial 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

VTOL AIRCRAFTSALKIND MJ.1973; A.S.T.M. SPEC. TECH. PUBL.; U.S.A.; DA. 1973; NO 524; PP. 76-107; BIBL. 17 REF.Serial Issue

SPACE STRUCTURESFOREST JD; CHRISTIAN JL.1973; A.S.T.M. SPEC. TECH. PUBL.; U.S.A.; DA. 1973; NO 524; PP. 134-162; BIBL. 17 REF.Serial Issue

ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT CONFERENCE PROCEEDINGS ON HIGH TEMPERATURE CORROSION OF AEROSPACE ALLOYS; LYNGBY; 19721973; A.G.A.R.D. CONF. PROC.; FR.; DA. 1973; NO 120; PP. (356 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

ADVANCED ROTORCRAFT. 39TH. MEETING OF THE FLIGHT MECHANICS PANEL OF A.G.A.R.D. I. HAMPTON, VIRGINIA, 20-23 SEPTEMBER 19711973; A.G.A.R.D. CONF. PROC.; FR.; DA. 1973; NO 121; PP. (233 P.); BIBL. DISSEM.Conference Paper

TESTING FOR PREDICTION OF MATERIAL PERFORMANCE IN STRUCTURES AND COMPONENTS. A SYMPOSIUM. I. II. ANAHEIM CALIF.-ATLANTIC CITY, N.J., 21-23 APRIL-29 JUNE-1 JULY 19711972; A.S.T.M. SPEC. TECH. PUBL.; U.S.A.; DA. 1972; NO 515; PP. (316 P.); BIBL. DISSEM.Conference Paper

MILITARY APPLICATION AND EXPERIENCE WITH COMPOSITESROSELIUS DA; WOOD HA.1971; S.A.E. TRANS.; U.S.A.; DA. 1971; VOL. 80; NO 3; PP. 1526-1535Serial 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