INSTRUMENT LANDING SYSTEMS = SYSTEMES D'ATTERRISSAGESANDERS LL; FRITCH VJ JR.1973; I.E.E.E. TRANS. COMMUNIC.; U.S.A.; DA. 1973; VOL. 21; NO 5; PP. 435-454; BIBL. 63 REF.Serial Issue

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

HUMAN FACTORS IN LOW WEATHER OPERATION OF TRANSPORT AIRCRAFT = FACTEURS HUMAINS DANS LA MISE EN OEUVRE D'AVIONS DE TRANSPORT PAR MAUVAIS TEMPSWILSON JW.1973; A.G.A.R.D. CONF. PROC.; FR.; DA. 1973; NO 114; PP. 20.1-20.5; (24TH TECH. MEET. AVIONICS PANEL AGARD: AUTOM. MANNED AEROSP. SYST.; DAYTON, OHIO; 1972)Conference 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

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

PROBLEME DER INTEGRATION VON FLUGFUEHRUNGSSYSTEM BEI NEUEN ANFLUGVERFAHREN = PROBLEME DE L'INTEGRATION DES INSTRUMENTS DE VOL ET DES SYSTEMES DE PILOTAGE DANS LES NOUVEAUX DISPOSITIFS DE DECOLLAGE ET D'ATTERRISSAGESCHANZER G.sdIN: 5. JAHRESTAG. DTSCH. GES. LUFT RAUMFAHRT; BERLIN; 1972; S.L.; DA. S.D.; PP. 1-20; H.T. 9; BIBL. 2 REF.Conference Paper

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

REDUCTION OF ILS ERRORS CAUSED BY BUILDING REFLECTIONS = REDUCTION D'ERREURS ILS CAUSEES PAR DES REFLEXIONS SUR DES BATIMENTSGHOSE RN.1973; J. AIRCR.; U.S.A.; DA. 1973; VOL. 10; NO 3; PP. 167-171; BIBL. 2 REF.Serial Issue

AN OPTIMAL CONTROL APPROACH TO TERMINAL AREA AIR TRAFFIC CONTROL = UNE APPROCHE PAR LE CONTROLE OPTIMAL DU PROBLEME DE CONTROLE DE TRAFIC AERIEN EN AIRE TERMINALESCHMIDT DK; SWAIM RL.1973; J. AIRCR.; U.S.A.; DA. 1973; VOL. 10; NO 3; PP. 181-188; BIBL. 17 REF.Serial Issue

A CASE HISTORY REPORT ON CARRIER LANDING SYSTEM. BURN. IN SOLVES RELIABILITY PROBLEMWOLFORD RE; CURRY C.1971; EVAL. ENGNG; U.S.A.; DA. 1971; VOL. 10; NO 5; PP. 16-19Serial Issue

ALLWETTERBETRIEB NACH KATEGORIE III UND/ODER ENTNEBELUNG = ATTERRISSAGE TOUT TEMPS EN CATEGORIE III ET/OU DISPERSION DU BROUILLARDCASTELL WD.1973; INTERNATION. VERKEHRSWES.; DTSCH.; DA. 1973; VOL. 25; NO 1; PP. 25-27; ABS. ANGLSerial Issue

TESTING AIRCRAFT WHEEL, TYRE AND BRAKE UNITS = L'ESSAI DES ROUES, DES PNEUMATIQUES ET DES UNITES DE FREINAGE DES AVIONS1973; MEASUR. AND CONTROL; G.B.; DA. 1973; VOL. 6; NO 4; PP. 139-140Serial Issue

A SYSTEM FOR THE PRECISE CALIBRATION OF AIR NAVIGATIONAL RECEIVERSSORGER GU.1972; I.E.E.E. TRANS. INSTRUMENT. MEASUR.; U.S.A.; DA. 1972; VOL. 21; NO 4; PP. 519-527; 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

COMMERCIAL TRANSPORT = TRANSPORT COMMERCIAL1973; SOC. EXPER. TEST PILOTS, TECH. REV.; U.S.A.; DA. 1973; VOL. 11; NO 2; PP. 82-157; BIBL. DISSEM.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

LOW-ALTITUDE ATMOSPHERIC TURBULENCE AROUND AN AIRPORT = TURBULENCE ATMOSPHERIQUE A BASSE ALTITUDE AUTOUR D'UN AEROPORTCASS SD; SCOGGINS JR; CHEVALIER HL et al.1973; J. AIRCR.; U.S.A.; DA. 1973; VOL. 10; NO 3; PP. 157-163; BIBL. 10 REF.Serial 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

DEVELOPMENT TESTING OF THE L-1011 INDEPENDENT LANDING MONITORHOLLIDAY G; GORHAM JA.1971; S.A.E. TRANS.; U.S.A.; DA. 1971; VOL. 80; NO 3; PP. 1592-1605; BIBL. 2 REF.Serial Issue