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METHODE DE CALCUL DES COEFFICIENTS AERODYNAMIQUES DE CERTAINS CORPS VOLUMINEUX DE SECTION TRANSVERSE QUELCONQUESKIBA GG; FEDOTOV BN.1977; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1977; NO 6; PP. 92-98; BIBL. 2 REF.Article

THE EFFECT OF THE AXIAL VELOCITY DENSITY RATIO ON THE AERODYNAMIC COEFFICIENTS OF COMPRESSOR CASCADESSTARKE J.1981; J. ENG. POWER; ISSN 0022-0825; USA; DA. 1981; VOL. 103; NO 1; PP. 210-219; BIBL. 32 REF.Article

AERODYNAMIC COEFFICIENTS IN GENERALIZED UNSTEADY THIN AIRFOIL THEORYWILLIAMS MH.1980; AIAA J.; ISSN 0001-1452; USA; DA. 1980; VOL. 18; NO 7; PP. 850-852; BIBL. 4 REF.Article

ON LIFTING SURFACES IN UNSTEADY FLOWJORDAN PF.1980; Z. ANGEW. MATH. MECH.; ISSN 0044-2267; DDR; DA. 1980; VOL. 60; NO 7; PP. T193-T194; BIBL. 1 REF.Article

CALCULATION OF NONLINEAR LIFT AND PITCHING MOMENT COEFFICIENTS FOR SLENDER WING-BODY COMBINATIONS.OTTO H.1974; J. AIRCR.; U.S.A.; DA. 1974; VOL. 11; NO 8; PP. 489-491; BIBL. 4 REF.Article

DE LA CONSTRUCTION D'UN MODELE D'INTERACTION INTERMOLECULAIRE LORS DE LA RESOLUTION DE L'EQUATION DE BOLTZMANN PAR LA METHODE DE MONTE-CARLOEROFEEV AI.1977; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1977; NO 6; PP. 171-175; BIBL. 9 REF.Article

ANALYSIS OF UNSTEADY PRESSURE MEASUREMENTS ON AN AEROFOIL SECTION WITH AN HARMONICALLY OSCILLATING, SLOTTED FLAPKIENAPPEL KARL; ROUND DAVID F.1980; D.F.V.L.R. FORSCH.-BER.; DEU; DA. 1980; VOL. 80; NO 22; 65 P.; ABS. GER; BIBL. 1 REF.Serial Issue

DETERMINATION OF AERODYNAMIC DRAG FROM RADAR DATALIESKE RF; MACKENZIE AM.sdIN: AIAA 2ND ATMOS. FLIGHT MECH. CONF. PALO ALTO, CALIF., 1972; S.L.; AM. INST. AERONAUT. ASTRONAUT.; DA. S.D.; PP. 1-5; BIBL. 6 REF.Conference Paper

PERFORMANCE D'UN BATEAU HYDROFOIL A VOILEMASUYAMA Y.1980; J. SOC. NAV. ARCHIT. JPN.; ISSN 0514-8499; JPN; DA. 1980-06; VOL. 147; PP. 154-167; ABS. ENG; BIBL. 12 REF.Article

A STUDY OF ARTILLERY SHELL DRIFT AT HIGH ANGLE OF FIRE USING SOLAR ASPECT SENSORSCOLLINGS WZ; LIESKE RF.sdIN: AIAA 2ND ATMOS. FLIGHT MECH. CONF. PALO ALTO, CALIF., 1972; S.L.; AM. INST. AERONAUT. ASTRONAUT.; DA. S.D.; PP. 1-10; BIBL. 10 REF.Conference Paper

RESOLUTION DU PROBLEME DE L'ECOULEMENT GAZEUX SUPERSONIQUE AUTOUR DE CORPS DE REVOLUTION, DANS LA THEORIE DES PETITES PERTURBATIONSVASIL'CHENKO VI; KUSAKIN SI.1977; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1977; NO 6; PP. 99-106; BIBL. 4 REF.Article

COUCHE LIMITE SUR UNE AILE DANS UN ECOULEMENT FORTEMENT TURBULENTJANOUR Z.1972; STROJN. CAS.; CESKOSL.; DA. 1972; VOL. 23; NO 6; PP. 499-511; ABS. RUSSE ANGL.; BIBL. 3 REF.Serial Issue

LIMITATIONS IN THE ACQUISITION OF NONLINEAR AERODYNAMIC COEFFICIENTS FROM FREE-OSCILLATION DATA BY MEANS OF THE CHAPMAN-KIRK TECHNIQUEHOLMES JE.sdIN: AIAA 2ND ATMOS. FLIGHT MECH. CONF. PALO ALTO, CALIF., 1972; S.L.; AM. INST. AERONAUT. ASTRONAUT.; DA. S.D.; PP. 1-4; BIBL. 3 REF.Conference Paper

CHAINE DE MESURE NUMERIQUE DE COEFFICIENTS DE PRESSION INSTATIONNAIRECHRISTOUX C; GRAVELLE A.1980; RECH. AEROSP.; ISSN 0034-1223; FRA; DA. 1980; NO 1; PP. 63-68; ABS. ENG; BIBL. 2 REF.Article

AN UNSTEADY VORTEX PANEL METHOD AND ITS APPLICATION TO AEROELASTIC CALCULATIONS OF A FIXED, THIN WING AND AN UNCONSTRAINED FLYING VEHICLE.ULV MAI H.1975; HELSINKI UNIV. TECHNOL., RES. PAPERS; FINL.; DA. 1975; NO 52; PP. 1-115; BIBL. 4 P.; (THESIS DOCT. TECHNOL.; HELSINKI UNIV. TECHNOL.; 1975)Thesis

INFLUENCE OF HINGE LINE GAP ON AERODYNAMIC FORCES ACTING ON A HARMONICALLY OSCILLATING THIN PROFILE IN AN INCOMPRESSIBLE FLOW. IIFILIPKOWSKI S; NOWAK M.1980; ARCH. MECH.; ISSN 0373-2029; POL; DA. 1980; VOL. 32; NO 4; PP. 535-548; ABS. POL/RUS; BIBL. 14 REF.Article

INFLUENCE OF HINGE LINE GAP ON AERODYNAMIC FORCES ACTING ON A HARMONICALLY OSCILLATING THIN PROFILE IN AN INCOMPRESSIBLE FLOW. IFILIPKOWSKI S; NOWAK M.1980; ARCH. MECH.; ISSN 0373-2029; POL; DA. 1980; VOL. 32; NO 4; PP. 517-534; ABS. POL/RUS; BIBL. 14 REF.Article

AERODYNAMISCHE BEIWERTE IN NATUERLICHER WINDSTROEMUNG = LES COEFFICIENTS AERODYNAMIQUES DANS L'ECOULEMENT NATUREL DU VENTNIEMANN HJ.1981; KONSTR. ING. BAU; ISSN 0023-3633; DEU; DA. 1981; NO 38-39; PP. 49-53; BIBL. 4 REF.Article

Method for estimating the aerodynamic coefficients of wind turbine blades at high angles of attackBEANS, E. W; JAKUBOWSKI, G. S.Journal of energy. 1983, Vol 7, Num 6, pp 747-749, issn 0146-0412Article

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