kw.\*:("TRAIN ATTERRISSAGE")
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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
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
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
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
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
AN EXPERIMENTAL INVESTIGATION OF AIRFRAME COMPONENT INTERFERENCE NOISE.BLOCK PJW.1977; IN: AEROSP. SCI. MEET. 15; LOS ANGELES, CALIF.; 1977; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. 1977; VOL. 48; PP. 1-9; H.T. 2; BIBL. 12 REF.Conference Paper
7 MW DRIVE FOR TESTING TYRES1972; ELECTR. TIMES; G.B.; DA. 1972; VOL. 162; NO 24; PP. 33Serial Issue
Dynamic response of landing gears on rough repaired runwayTING-WHAI LEE.SAE transactions. 1991, Vol 100, Num 1, pp 2569-2578, issn 0096-736X, 2Article
Monitoring of aircraft landing gear structureSCHMIDT, R. K.Aeronautical Journal. 2008, Vol 112, Num 1131, pp 275-278, issn 0001-9240, 4 p.Conference Paper
Undercarriage Lateral Tip-Over Criteria: A Parametric StudyHESLEHURST, Rikard Benton.Journal of aircraft. 2011, Vol 48, Num 6, pp 1825-1828, issn 0021-8669, 4 p.Article
Breaking the chain returning Concorde to service following the Paris accident: July 2000JUPP, J. A; BRITTON, J. R.Aeronautical Journal. 2003, Vol 107, Num 1073, pp 447-458, issn 0001-9240, 12 p.Article
The retractable airplane landing gear and the Northrop Anomaly': variation-selection and the shaping of technologyVINCENTI, W. G.Technology and culture. 1994, Vol 35, Num 1, pp 1-33, issn 0040-165XArticle
Mean flow features around the inline wheels of four-wheel landing gearLAZOS, Barry S.AIAA journal. 2002, Vol 40, Num 2, pp 193-198, issn 0001-1452Article
Composite Tube Exhibiting Large Deformation under BendingDERISI, Bijan; SUONG HOA; DUOSHENG XU et al.Journal of composite materials. 2010, Vol 44, Num 16, pp 2005-2020, issn 0021-9983, 16 p.Article