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Results 1 to 25 of 122

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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

REVIEW: AXIAL COMPRESSOR STALL PHENOMENAGREITZER EM.1980; J. FLUIDS ENG.; ISSN 0098-2202; USA; DA. 1980; VOL. 102; NO 2; PP. 134-151; BIBL. 80 REF.Article

THE INFLUENCE OF LOSSES ON THE EVALUATION OF THE "ROTATING STALL"MORAVEC Z.1979; CONFERENCE ON FLUID MACHINERY. 6/1979/BUDAPEST; HUN; BUDAPEST: AKAD. KIADO; DA. 1979; VOL. 2; PP. 735-742; BIBL. 4 REF.Conference Paper

NUMERICAL LIFTING LIME THEORY APPLIED TO DROOPED LEADING-EDGE WINGS BELOW AND ABOVE STALLANDERSON JD JR; CORDA S; VAN WIE DM et al.1980; J. AIRCR.; ISSN 0021-8669; USA; DA. 1980; VOL. 17; NO 12; PP. 898-904; BIBL. 20 REF.Article

VIBRATIONS DE MAQUETTES AU-DELA DU DECROCHAGE A BASSE VITESSEVAUCHERET X.1980; RECH. AEROSP.; ISSN 0034-1223; FRA; DA. 1980; NO 6; PP. 387-397; ABS. ENG; BIBL. 5 REF.Article

Modélisation du décrochage dynamique par équations différentielles = Dynamic stall modelling using differential equationsPETOT, D.La Recherche aérospatiale. 1989, Num 5, pp 59-72, issn 0034-1223, 14 p.Article

ETUDE EXPERIMENTALE DU FLOTTEMENT D'AUBES DE COMPRESSEURSSZECHENYI E.1983; RFM, REVUE FRANCAISE DE MECANIQUE; ISSN 0373-6601; FRA; DA. 1983; NO 2; PP. 33-36; ABS. ENGArticle

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

Evaluation of a stalled airfoil analysis programRUMSEY, C. L.Journal of aircraft. 1985, Vol 22, Num 2, pp 156-157, issn 0021-8669Article

Engineering analysis of drooped leading-edge wings near stallTAE HWAN CHO; ANDERSON, J. D. JR.Journal of aircraft. 1984, Vol 21, Num 6, pp 446-448, issn 0021-8669Article

EFFECT OF WAKE-TYPE NONUNIFORM INLET VELOCITY PROFILES ON FIRST APPRECIABLE STALL IN PLANE-WALL DIFFUSERSKAISER KF; MACDONALD AT.1980; J. FLUIDS ENG.; ISSN 0098-2202; USA; DA. 1980; VOL. 102; NO 3; PP. 285-289; BIBL. 16 REF.Article

TRANSONIC FLOW PAST A SYMMETRICAL AIRFOIL AT HIGH ANGLE OF ATTACKJOHNSON DA; BACHALO WD; OWEN FK et al.1981; J. AIRCR.; ISSN 0021-8669; USA; DA. 1981; VOL. 18; NO 1; PP. 7-14; BIBL. 18 REF.Article

STRAIGHT-WALLED, TWO-DIMENSIONAL DIFFUSERS-TRANSITORY STALL AND PEAK PRESSURE RECOVERYASHJAEE J; JOHNSTON JP.1980; J. FLUIDS ENG.; ISSN 0098-2202; USA; DA. 1980; VOL. 102; NO 3; PP. 275-282; BIBL. 18 REF.Article

GROWTH OF A PERTURBATION IN AN AXIAL FLOW COMPRESSORFABRI J.1979; J. ENG. POWER; ISSN 0022-0825; USA; DA. 1979; VOL. 101; NO 1; PP. 87-94; BIBL. 13 REF.Article

Experimental investigation of dynamic stall for a pitching airfoilDALEY, D. C; JUMPER, E. J.Journal of aircraft. 1984, Vol 21, Num 10, pp 831-832, issn 0021-8669Article

Dynamic stall inception correlation for airfoils undergoing constant pitch rate motionsSTRICKLAND, J. H; GRAHAM, G. M.AIAA journal. 1986, Vol 24, Num 4, pp 678-680, issn 0001-1452Article

Importance du décrochage dynamique dans les calculs aérodynamiques du rotor Darrieus = Dynamic stall behaviour in the aerodynamic calculations of the Darrieux rotorFRAUNIE, P; BEGUIER, C; PARASCHIVOIU, I et al.Journal de mécanique théorique et appliquée. 1985, Vol 4, Num 6, pp 785-804, issn 0750-7240Article

Modélisation du décrochage dynamique du profil NACA 0012 = Modeling the dynamic stall of the NACA 0012 profilePETOT, D.La Recherche aérospatiale. 1984, Num 6, pp 439-442, issn 0034-1223Article

DYNAMIC PRESSURE RESPONSE WITH STALL ON AXIAL FLOW COMPRESSOR ROTOR BLADESCOUSINS WT; O'BRIEN WF JR; SEXTON MR et al.1981; AEROSPACE SCIENCES MEETING. 19 /1981-01-12/SAINT LOUIS MO; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1981; 6 P.; BIBL. 9 REF.Conference Paper

A DISCRETE VORTEX METHOD FOR THE NON-STEADY SEPARATED FLOW OVER AN AIRFOILKATZ J.1981; J. FLUID MECH.; ISSN 0022-1120; GBR; DA. 1981; VOL. 102; PP. 315-328; BIBL. 23 REF.Article

DYNAMIC TOTAL HEAD LOSS CHARACTERISTIC FOR AN AXIAL COMPRESSOR ROTORSHARMA PB; RAILLY JW.1980; J. MECH. ENG. SCI.; ISSN 0022-2542; GBR; DA. 1980; VOL. 22; NO 6; PP. 269-276; BIBL. 13 REF.Article

VISUALISATION DES REGIMES INSTATIONNAIRES DES COMPRESSEURS ET DES POMPESPAULON J.1983; RFM, REVUE FRANCAISE DE MECANIQUE; ISSN 0373-6601; FRA; DA. 1983; NO 2; PP. 3-12; ABS. ENG; BIBL. 7 REF.Article

COMPRESSOR STABILITY ANALYSISBAGHDADI S; LUEKE JE.1982; J. FLUIDS ENG.; ISSN 0098-2202; USA; DA. 1982; VOL. 104; NO 2; PP. 242-249; BIBL. 12 REF.Article

CONCERNING DYNAMIC STALLSMITH FT.1982; AERONAUT. Q.; ISSN 0001-9259; GBR; DA. 1982; VOL. 33; NO 4; PP. 331-352; BIBL. 15 REF.Article

STALL FLUTTER OF LINEAR CASCADE IN COMPRESSIBLE FLOWKAJI S.1980; VIBRATIONS IN ROTATING MACHINERY. INTERNATIONAL CONFERENCE. 2/1980/CAMBRIDGE; GBR; LONDON: MECHANICAL ENGINEERING PUBLICATIONS; DA. 1980; PP. 209-214; BIBL. 5 REF.Conference Paper

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