THE EFFECTS OF LEADING EDGE MODIFICATIONS ON THE POST-STALL CHARACTERISTICS OF WINGSWINKELMANN AE; BARLOW JB; SAINI JK et al.1980; AEROSPACE SCIENCES MEETING. 18/1980/PASADENA CA; USA; NEW YORK: AIAA; DA. 1980; 15 P.; BIBL. 18 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

TECHNICAL EVALUATION REPORT/FLUID DYNAMICS PANEL SYMPOSIUM ON AERODYNAMIC CHARACTERISTICS OF CONTROL, NAPLES, MAY 14-17, 1979THOMAS HHBM ED.1980; FLUID DYNAMICS PANEL SYMPOSIUM ON AERODYNAMIC CHARACTERISTICS OF CONTROL/1979-05-14/NAPLES; FRA; PARIS: AGARD; DA. 1980; 15 P.; 30 CM; ISBN 92-835-1351-7; AGARD ADVISORY REPORT; 157;[; AGARD/AR-157]Conference Proceedings

SCRUTON NUMBER: A PROPOSALZDRAVKOVICH MM.1982; J. WIND ENG. IND. AERODYN.; ISSN 0167-6105; NLD; DA. 1982; VOL. 10; NO 3; PP. 263-265; BIBL. 19 REF.Article

Computation of insect hoveringWANG, Z. Jane.Mathematical methods in the applied sciences. 2001, Vol 24, Num 17-18, pp 1515-1521, issn 0170-4214Conference Paper

Post stall studies of untwisted varying aspect ratio Slades with NACA 44 XX series airfoil sectionsOSTOWARI, C; NAIK, D.Wind engineering. 1985, Vol 9, Num 3, pp 149-164, issn 0309-524XArticle

Stability in Ornithopter Longitudinal Flight DynamicsDIED, John M; GARCIA, Ephrahim.Journal of guidance, control, and dynamics. 2008, Vol 31, Num 4, pp 1157-1163, issn 0731-5090, 7 p.Article

Progress in analysis and prediction of dynamic stallCARR, L. W.Journal of aircraft. 1988, Vol 25, Num 1, pp 6-17, issn 0021-8669Article

SUBSONIC/TRANSONIC CONFIGURATION AERODYNAMICSKORNER HORST.1981; ; FRA; NEUILLY-SUR-SEINE: AGARD; DA. 1981; AGARD-AR/146; 14 P.; 30 CM; BIBL. 29 REF.; ISBN 92-835-1380-0Report

A PROPOS DE L'APPROXIMATION DES CARACTERISTIQUES AERODYNAMIQUES D'UNE AILE A VOLET RIGIDEVATOLIN AK; OVCHINNIKOV VA; PAVLOV VG et al.1979; IZVEST. VYSSH. UCHEBN. ZAVED., AVIAC. TEKH.; SUN; DA. 1979; NO 2; PP. 16-21; BIBL. 6 REF.Article

COEFFICIENT DE REMPLISSAGE DES OUVERTURES DANS LE ROTOR D'UNE SIRENE DYNAMIQUEYUDAEV VF.1979; IZVEST. VYSSH. UCHEBN. ZAVED., MASH.-STR.; SUN; DA. 1979; NO 4; PP. 96-100; BIBL. 2 REF.Article

The influence of negative work on optimal flapping flightJOHNSTON, Christopher O; MASON, William H; CHEOLHEUI HAN et al.Journal of mechanical science and technology. 2010, Vol 24, Num 12, pp 2441-2449, issn 1738-494X, 9 p.Article

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

The pitching delta wingMOHAMED GAD-EL-HAK; CHIH-MING HO.AIAA journal. 1985, Vol 23, Num 11, pp 1660-1665, issn 0001-1452Article

COMPRESSIBLE HELICOIDAL SURFACE THEORY FOR PROPELLER AERODYNAMICS AND NOISEHANSON DB.1983; AIAA JOURNAL; ISSN 0001-1452; USA; DA. 1983; VOL. 21; NO 6; PP. 881-889; BIBL. 30 REF.Article

Caractéristiques aérodynamiques et thermiques des corps tridimensionnels en étoile dans un gaz raréfiéBUNIMOVICH, A. I; KUZ'MENKO, V. I.Izvestiâ Akademii nauk SSSR. Mehanika židkosti i gaza. 1983, Num 4, pp 181-183, issn 0568-5281Article

THERMODYNAMIC EQUILIBRIUM-AIR CORRELATIONS FOR FLOWFIELD APPLICATIONSZOBY EV; MOSS JN.1982; AIAA J.; ISSN 0001-1452; USA; DA. 1982; VOL. 20; NO 6; PP. 849-854; BIBL. 32 REF.Article

CARACTERISTIQUES AERODYNAMIQUES DE CORPS PORTANTS POLYGONAUX AUX VITESSES SUPERSONIQUESMAZHUL II.1982; IZVESTIJA SIBIRSKOGO OTDELENIJA AKADEMII NAUK SSSR. SERIJA TEHNICESKIH NAUK; ISSN 0002-3434; SUN; DA. 1982; NO 3; PP. 53-59; BIBL. 8 REF.Article

AEROTHERMODYNAMIC BASE HEATING.INOUE Y; PAGE RH.1977; IN: AM. INST. AERONAUT. ASTRONAUT. THERMOPHYS. CONF. 12; ALBUQUERQUE, N. MEX.; 1977; NEW YORK; AIAA; DA. 1977; VOL. 726; PP. (8P.); BIBL. 16 REF.Conference Paper

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

DERIVATION OF THE FUNDAMENTAL EQUATION OF SOUND GENERATED BY MOVING AERODYNAMIC SURFACESAGGARWAL HR.1983; AIAA JOURNAL; ISSN 0001-1452; USA; DA. 1983; VOL. 21; NO 7; PP. 1048-1050; BIBL. 6 REF.Article

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

CATASTROPHIC LIFT FORCES ON RACING CARSHOWELL J.1981; J. WIND. ENG. IND. AERODYN.; ISSN 0167-6105; NLD; DA. 1981; VOL. 9; NO 1-2; PP. 145-154; BIBL. 4 REF.Conference Paper

EMPIRICAL ESTIMATES OF GUST LOADS ON FINITE WINGSPATEL MH.1981; AIAA J.; ISSN 0001-1452; USA; DA. 1981; VOL. 19; NO 12; PP. 1602-1604; BIBL. 7 REF.Article

WING-ALONE AERODYNAMIC CHARACTERISTICS AT HIGH ANGLES OF ATTACKSTALLINGS RL JR; LAMB M.1981; AEROSPACE SCIENCES MEETING. 19 /1981-01-12/SAINT LOUIS MO; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1981; 7 P.; BIBL. 6 REF.Conference Paper