OPTIMUM PERFORMANCE OF STATIC PROPELLERS AND ROTORS = PERFORMANCE OPTIMALE DES HELICES STATIQUES ET DES ROTORSWU JC; SIGMAN RK; GOORJIAN PM et al.1972; IN: DEV. THEOR. APPL. MECH. PROC. 6TH SOUTHEAST. CONF. TAMPA, FLA, 1972; TAMPA, FLA; 6TH SOUTHEAST. CONF. THEOR. APPL. MECH.; DA. 1972; VOL. 6; PP. 229-252; BIBL. 13 REF.Conference Proceedings

PARAMETRIC TRENDS & OPTIMIZATION. PRELIMINARY SELECTION OF CONFIGURATION. PROTOTYPE DESIGN & MANUFACTURE = TENDANCES PARAMETRIQUES ET OPTIMISATION. CHOIX PRELIMINAIRE D'UNE CONFIGURATION. CONCEPTION ET FABRICATION DU PROTOTYPEHUBER H.1973; AGARD-LS-63; FR.; DA. 1973; PP. 8.1-8.55; BIBL. 3 P. 1/2; (HELICOPTER AERODYN. DYN.; BRUSSELS; 1973)Conference Proceedings

INFLUENCE OF AIRFOILS ON STALL FLUTTER BOUNDARIES OF ARTICULATED HELICOPTER ROTORS = INFLUENCE DES PROFILS SUR LES LIMITES DE FLOTTEMENT DE DECROCHAGE DE ROTORS ARTICULES D'HELICOPTERESBENSON RG; DADONE LU; GORMONT RE et al.1973; J. AMER. HELICOPTER SOC.; U.S.A.; DA. 1973; VOL. 18; NO 1; PP. 36-46; BIBL. 1 REF.Serial Issue

VORTEX NOISE OF ISOLATED AIRFOILS = BRUIT D'ORIGINE TOURBILLONNAIRE DE PROFILS ISOLESPATERSON RW; VOGT PG; FINK MR et al.1973; J. AIRCR.; U.S.A.; DA. 1973; VOL. 10; NO 5; PP. 296-302; BIBL. 15 REF.Serial Issue

AEROSPATIALE PUMA1973; INTERAVIA; SUISSE; DA. 1973; VOL. 28; NO 5; PP. 535Serial Issue

THE ROLE OF AERODYNAMICS AND DYNAMICS IN MILITARY AND CIVILIAN APPLICATIONS OF ROTARY WING AIRCRAFT = LE ROLE DE L'AERODYNAMIQUE ET DE LA DYNAMIQUE DANS LES APPLICATIONS MILITAIRES ET CIVILES DES AVIONS A VOILURE TOURNANTEYAGGY PF.1973; AGARD-LS-63; FR.; DA. 1973; PP. 1.1-1.14; (HELICOPTER AERODYN. DYN.; BRUSSELS; 1973)Conference Proceedings

ANALYSIS OF TRANSMISSION FAILURE MODESBOWEN CW.1971; S.A.E. TRANS.; U.S.A.; DA. 1971; VOL. 80; NO 3; PP. 1626-1631; BIBL. 8 REF.Serial Issue

A NEW APPROACH TO HELICOPTER WEIGHT FRACTIONS = UNE NOUVELLE APPROCHE DU PROBLEME DES FRACTIONS DE POIDS POUR LES HELICOPTERESHOFFMANN TL; KAMPSCHAFER AR.1973; SOC. EXPER. TEST PILOTS, TECH. REV.; U.S.A.; DA. 1973; VOL. 11; NO 3; PP. 87-99Serial Issue

EQUATIONS DE LA DEFORMATION D'UNE PALE D'HELICE ET PROPRIETES ORTHOGONALES DE SES VIBRATIONS PROPRESLISS A YU.1972; IZVEST. VYSSH. UCHEBN. ZAVED., AVIAC. TEKH.; S.S.S.R.; DA. 1972; NO 4; PP. 56-66; BIBL. 7 REF.Serial Issue

AERODYNAMIC SOURCES OF ROTOR NOISE = SOURCES AERODYNAMIQUES DU BRUIT DES ROTORSCOX CR.1973; J. AMER. HELICOPTER SOC.; U.S.A.; DA. 1973; VOL. 18; NO 1; PP. 3-9; BIBL. 25 REF.Serial Issue

MEASUREMENT AND ANALYSIS OF ROTOR/PROPELLER NOISEIVES TR; LEVERTON JW.sdIN: CONF. REC. INTERPRETATION ENG. MEAS. PROC.; LONDON; 1972; LONDON; INST. MAR. ENG.; DA. S.D.; PP. 233-248 (9 P.); BIBL. 5 REF.Conference Proceedings

FLIGHT TESTING FOR PERFORMANCE AND FLYING QUALITIES = ESSAIS EN VOL DE PERFORMANCES ET DE QUALITES DE VOLMCKENZIE KT.1973; AGARD-LS-63; FR.; DA. 1973; PP. 9.1-9.15; (HELICOPTER AERODYN. DYN.; BRUSSELS; 1973)Conference Proceedings

A PERTURBATION SOLUTION OF HELICOPTER ROTOR FLAPPING STABILITY = UNE SOLUTION PAR PERTURBATION DU PROBLEME DE LA STABILITE DE BATTEMENT D'UN ROTOR D'HELICOPTEREJOHNSON W.1973; J. AIRCR.; U.S.A.; DA. 1973; VOL. 10; NO 5; PP. 257-258; BIBL. 4 REF.Serial Issue

FLAP-LAG STABILITY OF HELICOPTER ROTOR BLADES IN FORWARD FLIGHT.PETERS DA.1975; J. AMER. HELICOPTER SOC.; U.S.A.; DA. 1975; VOL. 20; NO 4; PP. 2-13; BIBL. 10 REF.Article

FIABILITE DES TRANSMISSIONS D'HELICOPTERESLIBEER JP.1973; AERONAUT. ET ASTRONAUT.; FR.; DA. 1973; NO 40; PP. 108-116; ABS. ANGL. ALLEMSerial Issue

IDENTIFICATION AND OPTIMIZATION OF AIRCRAFT DYNAMICS = IDENTIFICATION ET OPTIMISATION DE LA DYNAMIQUE D'UN AVIONNARENDRA KS; TRIPATHI SS.1973; J. AIRCR.; U.S.A.; DA. 1973; VOL. 10; NO 4; PP. 193-199; BIBL. 5 REF.Serial Issue

MILITARY PROGRAMS = PROGRAMMES MILITAIRES1973; SOC. EXPER. TEST PILOTS, TECH. REV.; U.S.A.; DA. 1973; VOL. 11; NO 2; PP. (82 P.); BIBL. 5 REF.Serial Issue

HEAVY LIFT HELICOPTER PROGRAM: AN ADVANCED TECHNOLOGY SOLUTION TO TRANSPORTATION PROBLEMS = PROGRAMME D'HELICOPTERE LOURD: UNE SOLUTION A TECHNOLOGIE AVANCEE AUX PROBLEMES DE TRANSPORTTENCER B; COSGROVE JP.1972; J. AIRCR.; U.S.A.; DA. 1972; VOL. 9; NO 11; PP. 753-758; BIBL. 6 REF.Serial Issue

GREASE LUBRICATION OF HELICOPTER TRANSMISSIONS = LUBRIFICATION PAR GRAISSE DES TRANSMISSIONS D'HELICOPTERESCHRISTIAN JB; SIMMONS BR.1973; IN: AM. SOC. LUBR. ENG. 28TH ANNU. MEET. TECH. PREPR.; CHICAGO, ILL.; 1973; PARK RIDGE, ILL.; AMER. SOC. LUBR. ENG.; DA. 1973; PP. 1-10Conference Paper

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

SYMPOSIUM ON HELIPORTS; 19721973; AERONAUT. J.; G.B.; DA. 1973; VOL. 77; NO 749; PP. 217-248; BIBL. DISSEM.Conference Paper

MANEUVERABILITY-THEORY AND APPLICATION = THEORIE DE LA MANOEUVRABILITE ET APPLICATIONWELLS CD; WOOD TL.1973; J. AMER. HELICOPTER SOC.; U.S.A.; DA. 1973; VOL. 18; NO 1; PP. 10-22; BIBL. 14 REF.Serial Issue

EFFECT OF PINS WITH FLATS AND RESIN BONDED POLYTETRAFLUORETHYLENE COATINGS ON THE FATIGUE STRENGTH OF LARGE PINNED CONNECTIONS MADE FROM ALLOY STEEL FV520BWHITE DJ.1970; INSTIT. MECH. ENGRS, PROC.; G.B.; DA. 1970; VOL. 185; PART 1; PP. 709-76; BIBL. 11 REF.Serial Issue

COMPLEX COORDINATES IN NEAR HOVERING ROTOR DYNAMICS = COORDONNEES COMPLEXES DANS LA DYNAMIQUE D'UN ROTOR EN VOL QUASI-STATIONNAIRECURTISS HC JR.1973; J. AIRCR.; U.S.A.; DA. 1973; VOL. 10; NO 5; PP. 289-296; BIBL. 11 REF.Serial 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