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Results 1 to 25 of 10105

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THE AERODYNAMIC EFFICIENCY OF WINDMILLS.LILLEY GM.1978; AERONAUT. QUART.; G.B.; DA. 1978; VOL. 29; NO 1; PP. 1-17; BIBL. 7 REF.Article

THE FLEXIBLE ENGINEER.CRABTREE LF.1977; Z. ANGEW. MATH. PHYS.; SCHWEIZ; DA. 1977; VOL. 28; NO 5; PP. 805-816; ABS. ALLEM.; BIBL. 6 REF.Article

RECOLLECTIONS FROM AN EARLIER PERIOD IN AMERICAN AERONAUTICS.JONES RT.1977; ANNU. REV. FLUID MECH.; U.S.A.; DA. 1977; VOL. 9; PP. 1-11Article

AERODYNAMIC BEHAVIOR OF THE VIKING ENTRY VEHICLE: GROUND TEST AND FLIGHT RESULTSKIRK DB; INTRIERI PF; SEIFF A et al.1978; J. SPACECR. ROCK.; USA; DA. 1978; VOL. 15; NO 4; PP. 208-212; BIBL. 12 REF.Article

PARACHUTE OPENING SHOCK CALCULATIONS WITH EXPERIMENTALLY ESTABLISHED INPUT FUNCTIONS.HEINRICH HG; SAARI DP.1978; J. AIRCR.; U.S.A.; DA. 1978; VOL. 15; NO 2; PP. 100-105; BIBL. 21 REF.Article

AERODYNAMIC AND THERMAL PROBLEMS AROUND AND INSIDE A DOME AND TELESCOPEROSCH J.1982; ASTROPHYS. SPACE SCI. LIBR.; ISSN 0067-0057; NLD; DA. 1982; VOL. 92; PP. 79-84; BIBL. 9 REF.Conference Paper

INVESTIGATION OF A SIDE FORCE DUE TO ABLATIONRAGSDALE WC; HORANOFF EV.1978; A.I.A.A. J. NEW YORK; USA; DA. 1978; VOL. 16; NO 9; PP. 1010-1011; BIBL. 2 REF.Article

PRELIMINARY COMPARISON OF MODEL AND PROTOTYPE WAKESLOGAN E; CAMP DW.1978; AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS AEROSPACE SCIENCES MEETING. 16/1978/HUNTSVILLE AL; USA; NEW YORK: AIAA; DA. 1978; 78-254; 10 P.; BIBL. 9 REF.Conference Paper

AN INVESTIGATION OF THE EFFECT OF BALLONET MOTIONS ON TETHERED AEROSTAT LONGITUDINAL DYNAMIC STABILITY.DE LAURIER J.1977; U.T.I.A.S. TECH. NOTE; CANADA; DA. 1977; NO 205; PP. (18P.); H.T. 8; BIBL. 10 REF.Serial Issue

SUBSONIC AERODYNAMICSDELAURIER JD; REID LD.1978; INST. AEROSPACE STUD., UNIV. TORONTO, ANNU. PROGR. REP.; CAN; DA. 1978; PP. 57-58; BIBL. 7 REF.Article

UEBER STOERFELDER BEWEGTER SINGULARITAETEN IN DER AERODYNAMIK UND AEROAKUSTIK = CHAMP DE PERTURBATION DES SINGULARITES MOBILES EN AERODYNAMIQUE ET EN AEROACOUSTIQUEDAS A.1978; D.F.U.L.R. FORSCH.-BER.; DEU; DA. 1978; VOL. 78; NO 16; PP. 1-94; ABS. ENG; BIBL. 7 P.Serial Issue

L'AERODYNAMIQUE DU LANCEUR ARIANNE.BOUCHET J; BEC R.1977; CENTRE NATION. ET. SPATIALES, NOTE TECH.; FR.; DA. 1977; NO 75; PP. 1-27; H.T. 22; ABS. ANGL.Serial Issue

SUR LA CONSTRUCTION DE PROFILS AERODYNAMIQUES VOISINS D'UN PROFIL DONNELAPORTE R.1978; J. MEC.; FRA; DA. 1978; VOL. 17; NO 2; PP. 207-229; ABS. ENG; BIBL. 20 REF.Article

PREDICTION OF ELASTIC-AIRPLANE LONGITUDINAL DYNAMICS FROM RIGID-BODY AERODYNAMICS.SWAIM RL; FULLMAN DG.1977; J. AIRCR.; U.S.A.; DA. 1977; VOL. 14; NO 9; PP. 868-873; BIBL. 7 REF.Article

A NOTE RELATED TO THE PRESSURE INSIDE AN INFLATING PARACHUTE CANOPY.PAYNE PR; BAND EGU.1977; AERONAUT. QUART.; G.B.; DA. 1977; VOL. 28; NO 4; PP. 271-277; BIBL. 5 REF.Article

GRIFFITH'S EARLY IDEAS ON TURBOMACHINERY AERODYNAMICS.HOWELL AR.1976; AERONAUT. J.; G.B.; DA. 1976; VOL. 80; NO 792; PP. 521-529; BIBL. 33 REF.Article

DYNAMIQUE DES SYSTEMES DE FREINAGE MOUBELOTSERKOVSKIJ SM; DNEPROV IV; PONOMAREV AT et al.1983; MEHANIKA TVERDOGO TELA; ISSN 0572-3299; SUN; DA. 1983; NO 1; PP. 47-54; BIBL. 7 REF.Article

COMPUTATIONAL AERODYNAMICS AND DESIGNBALLHAUS WF JR.1982; LECT. NOTES PHYS.; ISSN 0075-8450; DEU; DA. 1982; VOL. 170; PP. 1-20; BIBL. 10 REF.Conference Paper

OPTIMISATION DES STRUCTURES D'AVIONPETIAU C; LECINA G.1982; J. MEC. THEOR. APPL.; ISSN 0750-7240; FRA; DA. 1982; VOL. 1; NO 2; PP. 291-309; ABS. ENG; BIBL. 7 REF.Article

A FAST PSEUDO-TIME INTEGRATION SCHEME FOR THE STEADY TRANSONIC FLOW PROBLEMYURTSEVEN HO; KARACA C; ECER A et al.1982; COMPUT. METHODS APPL. MECH. ENG.; ISSN 0045-7825; NLD; DA. 1982; VOL. 34; NO 1-3; PP. 787-800; BIBL. 4 REF.Conference Paper

CONTRIBUTION TO ACCURATE MEASUREMENT OF AERODYNAMIC DRAG ON A MOVING VEHICLE FROM COAST-DOWN TESTS AND DETERMINATION OF ACTUAL ROLLING RESISTANCEROUSSILLON G.1981; J. WIND. ENG. IND. AERODYN.; ISSN 0167-6105; NLD; DA. 1981; VOL. 9; NO 1-2; PP. 33-48; BIBL. 11 REF.Conference Paper

SOUND SOURCES IN AERODYNAMICS: FACT AND FICTIONFFOWCS WILLIAMS JE.1981; AEROSPACE SCIENCES MEETING. 19 /1981-01-12/SAINT LOUIS MO; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1981; 11 P.; BIBL. 15 REF.Conference Paper

METHODE GENERALE DE CALCUL DES DISPOSITIFS D'ASPIRATION A PERFORATIONS DONT LA SURFACE LATERALE EST TOTALEMENT OU PARTIELLEMENT PERFOREEAKOBDZHANYAN AS.1981; IZV. VYSS. UCEBN. ZAVED., STROIT. ARHIT.; ISSN 0536-1052; SUN; DA. 1981; NO 2; PP. 126-132; BIBL. 4 REF.Article

ETUDES AERODYNAMIQUES DES COQUES ELLIPTIQUES TRONQUEESSMIRNOV AM; MILOVIDOV AS; KARTASHOV VE et al.1980; STROITEL. MEKH. RASCHET SOORUZH.; SUN; DA. 1980; NO 2; PP. 74-76; BIBL. 2 REF.Article

MODIFICATION OF WING SECTIONS TO OPTIMIZE TRANSONIC PERFORMANCELUNTZ A; BARNETT Y; DAREL I et al.1979; ISRAEL ANNUAL CONFERENCE ON AVIATION AND ASTRONAUTICS. 2/1979-02-28/TEL AVIV, HAIFA; ISR; HAIFA: AYALON OFFSET; DA. 1979; PP. 1-4; BIBL. 2 REF.Conference Paper

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