LE SYSTEME SYDACPRESLES M.1973; NAVIGATION; FR.; DA. 1973; VOL. 21; NO 82; PP. 165-174Serial Issue

SOLVING FLIGHT-PATH OPTIMIZATION PROBLEMS ON A MINICOMPUTER = RESOLUTION PAR ORDINATEUR DES PROBLEMES D'OPTIMISATION DES TRAJECTOIRES DE VOLTHOMASSON FY; COOK G.1973; ASTRONAUT. ACTA; G.B.; DA. 1973; VOL. 18; NO 1; PP. 45-51; ABS. ALLEM. FR.; BIBL. 1 REF.Serial 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

WIRKSAMKEITSUNTERSUCHUNGEN VON ANZEIGEN FUER DIE FLUGFUEHRUNG = ETUDES DE L'EFFICACITE DES INDICATEURS DE VOLBEYER R.1973; DTSCHE LUFT-U. RAUMFAHRT, FORSCH.-BER.; DTSCH.; DA. 1973; NO 3; PP. 1-30; ABS. ANGL.; BIBL. 2 P.Serial Issue

EIN BEITRAG ZUM SCHUTZ VON FLUGKOERPERN GEGENUEBER BLITZEINWIRKUNGEN = CONTRIBUTION A LA PROTECTION CONTRE LES ACTIONS DE LA FOUDRE SUR LES AERONEFSHEISE W.1972; TECH. MITT. A.E.G.-TELEFUNKEN; DTSCH.; DA. 1972; VOL. 62; NO 7; PP. 319-323; BIBL. 3 REF.Serial Issue

INTEGRATED ENGINE DIAGNOSTIC AND DISPLAYS FOR NAVY AIRCRAFT OF THE 1980'SPISCOPO PF.sdIN: AM. INST. AERONAUT. ASTRONAUT. SOC. AUTOMOT. ENG. 8TH JOINT PROPUL. SPEC. CONF.; NEW ORLEANS, LA.; 1972; NEW YORK; A.I.A.A.; DA. S.D.; NO 1084; PP. 1-5Conference Paper

MAN-MACHINE CONSIDERATIONS IN THE DEVELOPMENT OF A COCKPIT FOR AN ADVANCED TACTICAL FIGHTER = CONSIDERATIONS HOMME-MACHINE DANS LA MISE AU POINT D'UN COCKPIT POUR UN AVION DE COMBAT TACTIQUE AVANCEPREMSELAAR SJ; FREARSON DE.1973; A.G.A.R.D. CONF. PROC.; FR.; DA. 1973; NO 114; PP. 24.1-24.30; (24TH TECH. MEET. AVIONICS PANEL AGARD: AUTOM. MANNED AEROSP. SYST.; DAYTON, OHIO; 1972)Conference Paper

MANEUVER LOAD CONTROL AND RELAXED STATIC STABILITY APPLIED TO A CONTEMPORARY FIGHTER AIRCRAFT = APPLICATION A UN AVION DE COMBAT CONTEMPORAIN DU CONTROLE DE CHARGE DE MANOEUVRE ET DE LA RELAXATION DE STABILITE STATIQUEANDERSON DC; BERGER RL; HESS JR JR et al.1973; J. AIRCR.; U.S.A.; DA. 1973; VOL. 10; NO 2; PP. 112-120; BIBL. 2 REF.Serial 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

RAM AIR TURBINESMORRIS PW.1973; AIRCR. ENGNG; G.B.; DA. 1973; VOL. 45; NO 2; PP. 24-30 (3 P.)Serial Issue

CHARACTERISTICS OF AN EJECTOR-TYPE ENGINE SIMULATOR FOR STOL MODEL TESTING = CARACTERISTIQUES D'UN SIMULATEUR DE MOTEUR DU TYPE A EJECTION POUR L'ESSAI DE MODELES D'ADACNICOLOFF GB; WEBER HA.sdIN: AIAA 7TH AERODYN. TEST. CONF. PALO ALTO, CALIF., 1972; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. S.D.; NO 993; PP. 1-8; BIBL. 3 REF.Conference Paper

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

DEVELOPMENT OF CRASH-SAFE TURBINE FUELS = DEVELOPPEMENT DE COMBUSTIBLES DE SECURITE EN CAS D'ACCIDENT POUR TURBINESRUSSELL RA JR; SALMON RF.1971; IN: GAS TURBINE FLUIDS ENG. CONF. PROD. SHOW. SAN FRANCISCO, CALIF., 1972; HEADQUARTERS; A.S.M.E.; DA. 1971; VOL. 28; PP. 1-15; BIBL. 15 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

STATUS REPORT ON AIRCRAFT AND AIRPORTS AS SOURCES OF POLLUTIONSALLEE GP.1971; S.A.E. TRANS.; U.S.A.; DA. 1971; VOL. 80; PART 2; PP. 1329-1335; BIBL. 5 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

A STUDY OF HALON 1301 (CBRF₃) TOXICITY UNDER SIMULATED FLIGHT CONDITIONS = ETUDE DE LA TOXICITE DE L'HALON 1301 (CBRF₃) DANS DES CONDITIONS DE VOL SIMULECALL DW.1973; AEROSPACE MED.; U.S.A.; DA. 1973; VOL. 44; NO 2; PP. 202-204; BIBL. 11 REF.Serial Issue

Unified algebraic approach to approximation of lateral-directional modes and departure criteriaMENGALI, Giovanni; GIULIETTI, Fabrizio.Journal of guidance, control, and dynamics. 2004, Vol 27, Num 4, pp 724-728, issn 0731-5090, 5 p.Article

First and Second Law Analysis of Future Aircraft EnginesGRÖNSTEDT, Tomas; IRANNEZHAD, Mohammad; XU LEI et al.Journal of engineering for gas turbines and power. 2014, Vol 136, Num 3, issn 0742-4795, 031202.1-031202.10Article

Lateral-Directional Aircraft Dynamics Under Static Moment NonlinearityTIAUW HIONG GO.Journal of guidance, control, and dynamics. 2009, Vol 32, Num 1, pp 305-309, issn 0731-5090, 5 p.Article

The AIRBUS on-ground transport aircraft benchmarkJEANNEAU, Matthieu.Nonlinear analysis and synthesis techniques for aircraft control. Lecture notes in control and information sciences. 2007, pp 3-24, issn 0170-8643, isbn 3-540-73718-9, 1Vol, 22 p.Book Chapter