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Results 1 to 25 of 1135

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EFFETTO DELLO SPESSORE NEL CALCOLO DI FORZE AERODINAMICHE GENERALIZZATE SU UN' ALA OSCILLANTE. = EFFET DE L'EPAISSEUR SUR LE CALCUL DES FORCES AERODYNAMIQUES GENERALISEES SUR UNE AILE OSCILLANTESANTINI P; CARLINI O; OGNIBENE L et al.sdIN: SATELL. METEOROL. RISORSE TERREST. TECNOL. SPEC. COLLAB. INT. ATTI XIV CONV. INT. SPAZIO; ROMA; 1974; ROMA; RASSEGNA INT. ELETTRON. NUCL. AEROSP.; DA. S.D.; PP. 153-159; ABS. ANGL.; BIBL. 3 REF.Conference Paper

On the convergence of unsteady generalized aerodynamic forcesROWE, W. S; CUNNINGHAM, H. J.Journal of aircraft. 1984, Vol 21, Num 6, pp 420-427, issn 0021-8669Article

Application of diverging motions to calculate loads for oscillating motionsHOUNJET, M. H. L.AIAA journal. 1986, Vol 24, Num 10, pp 1723-1725, issn 0001-1452Article

Trigonometric models for large-angle aerodynamic force coefficientsBARRON, Roger L.Journal of guidance, control, and dynamics. 2003, Vol 26, Num 5, pp 825-827, issn 0731-5090, 3 p.Article

Optimization of airplane wing structures under landing loadsRAO, S. S.Computers & structures. 1984, Vol 19, Num 5-6, pp 849-863, issn 0045-7949Article

Endommagement par fatigue des structures élancées en béton armé soumises au vent aléatoire = Fatigue damage of slander reinforced concrete structures submitted to the random windBressolette, Philippe; Lemaire, Maurice.1989, 113 p.Thesis

Calculation of the aerodynamic forces on automotive lifting surfacesKATZ, J.Journal of fluids engineering. 1985, Vol 107, Num 4, pp 438-443, issn 0098-2202Article

Extension of the Blasius force theorem to subsonic speedsBARSONY-NAGY, A.AIAA journal. 1985, Vol 23, Num 11, pp 1811-1812, issn 0001-1452Article

Abschätzung von stochastischen Böenlasten unter Berücksichtigung instationärer Luftkräfte = Détermination de charges stochastiques en rafale dans le cas de forces de vent instationnaires = Estimation of unsteady aerodynamic loads in turbulenceSCHÄNZER, G.Zeitschrift für Flugwissenschaften und Weltraumforschung. 1985, Vol 9, Num 3, pp 167-178, issn 0342-068XArticle

Airfoil shape and thickness effects on transonic airloads and flutterBLAND, S. R; EDWARDS, J. W.Journal of aircraft. 1984, Vol 21, Num 3, pp 209-217, issn 0021-8669Article

Preliminary supersonic analysis methods including high angle of attackPITTMAN, J. L.Journal of aircraft. 1983, Vol 20, Num 9, pp 784-790, issn 0021-8669Article

DETERMINATION DES MOMENTS DES FORCES AERODYNAMIQUES S'EXERCANT SUR LES CORPS TRIDIMENSIONNELS SOUMIS A UN ECOULEMENT DANS LES CONDITIONS DE LA LOI DE LOCALISATIONVOROTYNTSEV MA; SAZONOVA NI.1976; VEST. MOSKOV. UNIV., 1; S.S.S.R.; DA. 1976; VOL. 31; NO 1; PP. 104-109; ABS. ANGL.; BIBL. 5 REF.Article

BERICHT UEBER DIE SITZUNG DES DGLR-FACHAUSSCHUSSES 3.4 VERSUCHSWESEN IN DER STROEMUNGSMECHANIK AM 5.6.1973 IN BREMEN. DIE MESSUNG VON TEILKRAEFTEN AN WINDKANALMODELLEN. = RAPPORT DU CONGRES DU COMITE SCIENTIFIQUE 3.4 DU DGLR SUR "LES TECHNIQUES EXPERIMENTALES DE LA MECANIQUE DES FLUIDES", DU 5 JUIN 1973 A BREME. MESURE DES FORCES SUR LES PARTIES DES MODELES MIS EN SOUFFLERIE AERODYNAMIQUE)EWALD B; KOPPENWALLNER G.1975; DTSCHE LUFT-U. RAUMFAHRT, MITT.; DTSCH.; DA. 1975; VOL. 75; NO 2; PP. 1-198; ABS. ANGLArticle

The use of multipoles for calculating the aerodynamic interference between bodies of revolutionCHRISTOPHER, P. A. T; SHAW, C. T.Journal of aircraft. 1984, Vol 21, Num 9, pp 673-679, issn 0021-8669Article

Active control of aerofoil flutterHUANG, X. Y.AIAA journal. 1987, Vol 25, Num 8, pp 1126-1132, issn 0001-1452Article

The numerical solution of flow around a rotating circular cylinder in uniform shear flowYOSHINO, F; HAYASHI, T.Bulletin of the JSME. 1984, Vol 27, Num 231, pp 1850-1857, issn 0021-3764Article

On the universal aerodynamic relations following from the Newtonian theoryNIKITIN, N. D.Fluid dynamics. 1998, Vol 33, Num 6, pp 933-935, issn 0015-4628Article

Atmospheric turbulence with respect to moving ground vehiclesCOOPER, R. K.Journal of wind engineering and industrial aerodynamics. 1984, Vol 17, Num 2, pp 215-238, issn 0167-6105Article

Aerohydrodynamic concentration of quartz sandsBROVTSYN, A. K; CHERSHNEVA, G. S.Refractories and industrial ceramics. 1998, Vol 39, Num 1-2, pp 67-69, issn 1083-4877Article

Aerodynamic indicial response and stability derivatives of a rotor annulusMENGLE, V. G.Journal of vibration, acoustics, stress, and reliability in design. 1988, Vol 110, Num 2, pp 178-184, issn 0739-3717Article

Unsteady transonic flow over cascade bladesSURAMPUDI, S. P; ADAMCZYK, J. J.AIAA journal. 1986, Vol 24, Num 2, pp 293-302, issn 0001-1452Article

Flutter analysis using nonlinear aerodynamic forcesUEDA, T; DOWELL, E. H.Journal of aircraft. 1984, Vol 21, Num 2, pp 101-109, issn 0021-8669Article

Reverse-flow theorem applied to subsonic unsteady aerodynamic forcesLOTTATI, I.Journal of aircraft. 1986, Vol 23, Num 1, pp 95-96, issn 0021-8669Article

THE EFFECT OF TRAILING-EDGE STRIPS ON THE UNSTEADY AERODYNAMIC FORCES ON A CONTROL SURFACELONG G; FARRELL PA.1980; AERONAUT. J.; ISSN 0001-9240; GBR; DA. 1980; VOL. 84; NO 838; PP. 388-391; BIBL. 5 REF.Article

CALCUL ANALYTIQUE DES CARACTERISTIQUES AERODYNAMIQUES DE CORPS DE REVOLUTION DANS LES CONDITIONS DE LA LOI DE LOCALITEBUNIMOVICH AI; CHISTOLINOV VG.1975; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1975; NO 5; PP. 94-100; BIBL. 6 REF.Article

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