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METHODES DE CLASSIFICATION DES SYSTEMES NON LINEAIRES DES TRAINS D'ATTERRISSAGE D'AVIONSPRINC J.1972; STROJN. CAS.; CESKOSL.; DA. 1972; VOL. 23; NO 6; PP. 592-610; ABS. RUSSE ANGL.; BIBL. 12 REF.Serial Issue

MODERN LANDING IMPACT LOAD CALCULATIONS AND OLD FASHIONED REQUIREMENTSYFF J.sdIN: 8TH CONGR. INT. COUNC. AERONAUT. SCI.; AMSTERDAM; 1972; NEW YORK; AM INST. AERONAUT. ASTRONAUT.; DA. S.D.; VOL. 31; PP. 1-9; BIBL. 7 REF.Conference Paper

THEORIE DES OSCILLATIONS D'UN AVIONLOBAS LG.1973; DOP. AKAD. NAUK U.R.S.R., A; S.S.S.R.; DA. 1973; VOL. 36; NO 3; PP. 258-262; ABS. ANGL. RUSSE; BIBL. 3 REF.Serial Issue

OPTIMIZATION OF COMMERCIAL TRANSPORT AIRPLANE STOPPING SYSTEMS = OPTIMISATION DES SYSTEMES D'ARRET DES AVIONS DE TRANSPORT COMMERCIAUXMEREDITH DB; HAINLINE BC.1972; IN: SOC. AUTOMOT. ENG. NATL. AEROSP. ENG. MANUF. MEET.; SAN DIEGO, CALIF.; 1972; NEW YORK; SOC. AUTOMOT. ENG.; DA. 1972; VOL. 872; PP. 1-10; BIBL. 3 REF.Conference Paper

TIRE DEVELOPMENT BY DEDICATED INVOLVEMENTSAVIERS H.1972; IN: SOC. AUTOMOT. ENG. NATL. AEROSP. ENG. MANUF. MEET.; SAN DIEGO, CALIF.; 1972; NEW YORK; SOC. AUTOMOT. ENG.; DA. 1972; VOL. 869; PP. 1-10Conference Paper

ANTISKID AND MODERN AIRCRAFT = ANTIDERAPAGE ET AVIATION MODERNEHIRZEL EA.1972; IN: SOC. AUTOMOT. ENG. NATL. AEROSP. ENG. MANUF. MEET.; SAN DIEGO, CALIF.; 1972; NEW YORK; SOC. AUTOMOT. ENG.; DA. 1972; VOL. 868; PP. 1-6Conference Paper

KNEELING LANDING GEAR. THE C5 VARIABLE GEOMETRY DEVELOPMENT = TRAIN D'ATTERRISSAGE "AGENOUILLABLE". MISE AU POINT D'UNE GEOMETRIE VARIABLE POUR LE C-51973; AIRCR. ENGNG; G.B.; DA. 1973; VOL. 45; NO 3; PP. 18-24 (3 P.)Serial Issue

ANALYSIS OF LEGGED LANDERS FOR THE SURVIVABLE SOFT LANDING OF INSTRUMENT PAYLOADS = ANALYSE D'ATTERRISSEURS MUNIS DE JAMBES DESTINES A L'ATTERRISSAGE EN DOUCEUR ET SANS DOMMAGE DE CHARGES UTILES CONSTITUEES D'INSTRUMENTSLAURENSON RM; MELLIERE RA; MCGEHEE JR et al.1973; J. SPACECR. ROCK.; U.S.A.; DA. 1973; VOL. 10; NO 3; PP. 208-214; BIBL. 6 REF.Serial Issue

VIBRATIONS OF AN EULER BEAM WITH A SYSTEM OF DISCRETE MASSES, SPRINGS AND DASHPOTS = VIBRATIONS D'UNE POUTRE D'EULER AVEC SYSTEME DE MASSES DISCRETES, RESSORTS ET AMORTISSEURSRAVAGHAN KS; SUNDARARAJAN V.1973; J. AIRCR.; U.S.A.; DA. 1973; VOL. 10; NO 3; PP. 190-192; BIBL. 6 REF.Serial Issue

COST YOUR BRAKES DOWN = REDUISEZ LE COUT DE VOS FREINSROSBACK RL.1972; IN: SOC. AUTOMOT. ENG. NATL. AEROSP. ENG. MANUF. MEET.; SAN DIEGO, CALIF.; 1972; NEW YORK; SOC. AUTOMOT. ENG.; DA. 1972; VOL. 867; PP. 1-6; BIBL. 5 REF.Conference Paper

POWERED WHEELS. A CONCEPT FOR PARKING AND TAXIING OF COMMERCIAL TRANSPORT AIRPLANESHAINLINE BC; SELLEREITE BK; SWANKE KV et al.1971; S.A.E. TRANS.; U.S.A.; DA. 1971; VOL. 80; NO 3; PP. 1617-1625; BIBL. 8 REF.Serial Issue

AIRCRAFT LANDING SIMULATOR TESTS BRAKES AND TYRES SIMULTANEOUSLY1973; ELECTR. REV.; G.B.; DA. 1973; VOL. 192; NO 18; PP. 638-639Serial Issue

CANTILEVER AIRCRAFT TIRES. MORE THAN A BREAK FOR BRAKESWOODALL WR.1972; IN: SOC. AUTOMOT. ENG. NATL. AEROSP. ENG. MANUF. MEET.; SAN DIEGO, CALIF.; 1972; NEW YORK; SOC. AUTOMOT. ENG.; DA. 1972; VOL. 870; PP. 1-9; BIBL. 1 REF.Conference Paper

NEW DYNAMOMETER FACILITY1973; TECH AIR; G.B.; DA. 1973; VOL. 29; NO 4; PP. 5-7Serial Issue

A MECHANIZED EDDY CURRENT SCANNING SYSTEM FOR AIRCRAFT STRUTS = SYSTEME D'OBSERVATION MECANISE PAR COURANT DE FOUCAULT POUR LES LONGERONS D'AVIONSREEVES CR.1973; MATER. EVALUAT.; U.S.A.; DA. 1973; VOL. 31; NO 3; PP. 48-52Serial Issue

BERYLLIUM BRAKE EXPERIENCE ON THE C-5A AIRPLANEGILSON RD.1971; S.A.E. TRANS.; U.S.A.; DA. 1971; VOL. 80; NO 3; PP. 1536-1544; BIBL. 4 REF.Serial Issue

DESIGN AND SIMULATION OF AN AIRCRAFT BRAKE USING A DIGITAL COMPUTER = CONCEPTION ET SIMULATION D'UN SYSTEME DE FREINAGE POUR AVIONS A L'AIDE D'UN ORDINATEURCLARIDGE JS.1973; AERONAUT. J.; G.B.; DA. 1973; VOL. 77; NO 747; PP. 136-147; BIBL. 7 REF.Serial Issue

ATTERRISSEURS D'AVION A COUSSIN D'AIRBRUNER G; LAURENT D.1973; AERONAUT. ET ASTRONAUT.; FR.; DA. 1973; NO 39; PP. 93-109; ABS. ANGL. ALLEM.; BIBL. 3 REF.Serial Issue

NON-STEADY-STATE THERMAL ANALYSIS OF A ROLLING AIRCRAFT TIRE = ANALYSE THERMIQUE EN REGIME NON STATIONNAIRE D'UN PNEUMATIQUE D'AVION EN ROULEMENTTRIVISONNO NM.1972; IN: SOC. AUTOMOT. ENG. NATL. AEROSP. ENG. MANUF. MEET.; SAN DIEGO, CALIF.; 1972; NEW YORK; SOC. AUTOMOT. ENG.; DA. 1972; VOL. 871; PP. 1-24; BIBL. 2 REF.Conference Paper

MODELLUNTERSUCHUNGEN ZUR BESTIMMUNG DES LAERMANTEILS VON FLUGZEUGFAHRWERKSCHACHKONFIGURATIONEN AM FLUGZEUGEIGENGERAUESCH = ETUDES SUR MODELE POUR LA DETERMINATION DE LA CONTRIBUTION DES CONFIGURATIONS DU PUITS DU TRAIN D'ATTERRISSAGE AU BRUIT PROPRE DES AVIONSDOBRZYNSKI W.1976; IN: FORTSCH. AKUST. TAG. DAGA'76.5.PLENARVORTR. KURZREF., HEIDELBERG; 1976; DUSSELDORF; VDI-VERLAG; DA. 1976; PP. 327-330; BIBL. 5 REF.Conference Paper

FURTHER DEVELOPMENTS IN SURFACE EFFECT TAKEOFF AND LANDING SYSTEMS CONCEPTS. A MULTICELL SYSTEM = DEVELOPPEMENTS SUPPLEMENTAIRES DANS LES CONCEPTS DE SYSTEMES DE DECOLLAGE ET D'ATTERRISSAGE A EFFET DE SURFACE. UN SYSTEME A PLUSIEURS CELLULESWILSON FW.1973; CANAD. AERONAUT. SPACE J.; CANADA; DA. 1973; VOL. 19; NO 3; PP. 121-128; BIBL. 2 REF.Serial Issue

FURTHER DEVELOPMENTS IN SURFACE EFFECT TAKEOFF AND LANDING SYSTEM CONCEPTS. APPLICATION TO HIGH PERFORMANCE AIRCRAFT = DEVELOPPEMENTS SUPPLEMENTAIRES DANS LES CONCEPTS DE SYSTEME DE DECOLLAGE ET ATTERRISSAGE A EFFET DE SURFACE. APPLICATION AUX AVIONS A HAUTES PERFORMANCESJOHNSON AE; MAGUIRE WB.1973; CANAD. AERONAUT. SPACE J.; CANADA; DA. 1973; VOL. 19; NO 3; PP. 109-119Serial Issue

STOL AIRCRAFT FLIGHT AND LANDING AREA CONSIDERATIONSRIEBE JM.1973; PROC. AMER. SOC. CIV. ENGRS, TRANSPORT. ENGNG J. A.S.C.E.; U.S.A.; DA. 1973; VOL. 99; NO 2; PP. 339-351; BIBL. 13 REF.Serial Issue

AIR CUSHION TECHNOLOGY: THE PROSPECTS FOR CANADIAN INDUSTRY = TECHNOLOGIE DU COUSSIN D'AIR: LES PERSPECTIVES POUR L'INDUSTRIE CANADIENNESULLIVAN PA.1973; CANAD. AERONAUT. SPACE J.; CANADA; DA. 1973; VOL. 19; NO 2; PP. 37-52; BIBL. 34 REF.Serial Issue

HYDROMECHANICAL DYNAMICS OF AIRCRAFT LANDING GEARALLEN RR.1981; FLUIDICS QUARTERLY; ISSN 0015-4687; USA; DA. 1981 PUBL. 1982; VOL. 13; NO 4; PP. 57-78; BIBL. 22 REF.Article

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