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ESTIMATION OF AERODYNAMICS FOR SLENDER BODIES ALONE AND WITH LIFTING SURFACES AT ALPHA 'S FROM 0O TO 90OJORGENSEN LH.1973; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1973; VOL. 11; NO 3; PP. 409-412; BIBL. 7 REF.Serial Issue

ACTIVE CONTROL OF ASYMMETRIC VORTEX EFFECTSFIDLER JE.1980; AEROSPACE SCIENCES MEETING. 18/1980/PASADENA CA; USA; NEW YORK: AIAA; DA. 1980; 11 P.; BIBL. 8 REF.Conference Paper

ACTIVE CONTROL OF ASYMMETRIC VORTEX EFFECTSFIDLER JE.1981; J. AIRCR.; ISSN 0021-8669; USA; DA. 1981; VOL. 18; NO 4; PP. 267-272; BIBL. 8 REF.Article

INTEGRALGLEICHUNGEN ZUR BERECHNUNG DER UMSTROEMUNG BESCHLEUNIGTER SCHLANKER KOERPER FUER M1. = EQUATIONS INTEGRALES POUR LE CALCUL DE L'ECOULEMENT AUTOUR DE CORPS ELANCES ACCELERES POUR M1BALLMANN J.1975; Z. ANGEW. MATH. MECH.; DTSCH.; DA. 1975; VOL. 55; NO 4; PP. 114-115; BIBL. 3 REF.; (WISS. JAHRESTAG. GES. ANGEW. MATH. MECH. VORTR.; BOCHUM; 1974)Conference Paper

COMMENT ON "APPROXIMATE CALCULATION OF VORTEX TRAJECTORIES OF SLENDER BODIES AT INCIDENCE". REPLY BY AUTHOR TO W.L. OBERKAMPFOBERKAMPF WL; WEIHS D.1983; AIAA JOURNAL; ISSN 0001-1452; USA; DA. 1983; VOL. 21; NO 2; PP. 317-318; BIBL. 10 REF.Article

INTEGRAL APPROXIMATION FOR SLENDER-BODY SHOCK SHAPES IN HYPERSONIC FLOW.FIORINO TD; RASMUSSEN ML.1974; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1974; VOL. 12; NO 2; PP. 1735-1737; BIBL. 8 REF.Article

HYPERSONIC FLOW OVER BLUNTED SLENDER WEDGES.MURTHY AV.1974; J. AIRCR.; U.S.A.; DA. 1974; VOL. 11; NO 4; PP. 249-251; BIBL. 9 REF.Article

REVIEW OF VORTEX-INDUCED ASYMMETRIC LOADS. IIERICSSON LE; REDING JP.1981; Z. FLUGWISS. WELTRAUMFORSCH.; ISSN 0342-068X; DEU; DA. 1981; VOL. 5; NO 6; PP. 349-366; ABS. GER; BIBL. 94 REF.Article

HIGH ANGLE-OF-ATTACK AERODYNAMICS ON A SLENDER BODY WITH A JET PLUME.NELSON RC; FLEEMAN EL.1975; J. SPACECR. ROCK.; U.S.A.; DA. 1975; VOL. 12; NO 1; PP. 12-16; BIBL. 8 REF.Article

UNIFORM ASYMPTOTIC SOLUTIONS FOR POTENTIAL FLOW ABOUT A SLENDER BODY OF REVOLUTION.GEER J.1975; J. FLUID MECH.; G.B.; DA. 1975; VOL. 67; NO 4; PP. 817-827; BIBL. 8 REF.Article

NON-LINEARITE DANS LA PORTANCE DE CORPS ELANCES EN INCIDENCE. INTRODUCTION D'UN NOUVEAU MODELE DE COUCHE TOURBILLONNAIREMATSUMURA K; TANAKA I; SAKUMA S et al.1982; J. SOC. NAVAL ARCHIT. JPN.; ISSN 0514-8499; JPN; DA. 1982-07; VOL. 151; PP. 65-74; ABS. ENG; BIBL. 17 REF.Article

SIDE FORCES ON UNYAWED SLENDER INCLINED AERODYNAMIC BODIES.KAO HC.1975; J. AIRCR.; U.S.A.; DA. 1975; VOL. 12; NO 3; PP. 142-150; BIBL. 15 REF.Article

ON BOUNDARY VALUE PROBLEMS FOR THE DOMAIN EXTERIOR TO A THIN OR SLENDER REGIONHOMENTCOVSCHI D.1983; ZEITSCHRIFT FUER ANGEWANDTE MATHEMATIK UND PHYSIK; ISSN 0044-2275; CHE; DA. 1983; VOL. 34; NO 3; PP. 322-333; ABS. FRE; BIBL. 24 REF.Article

THE DIFFRACTION OF A SHOCK WAVE BY A SLENDER BODY.MORGAN K.1975; Z. ANGEW. MATH. PHYS.; SCHWEIZ; DA. 1975; VOL. 26; NO 1; PP. 13-29; ABS. ALLEM.; BIBL. 7 REF.Article

CLASSE DE SOLUTIONS DE SIMILITUDE DES PROBLEMES D'ECOULEMENT HYPERSONIQUE DES CORPS DE REVOLUTION POREUXANTONOV AM; ZAJTSEV AV.1974; PRIKL. MEKL., U.S.S.R.; S.S.S.R.; DA. 1974; VOL. 10; NO 12; PP. 89-94; BIBL. 8 REF.Article

SCATTERING BY SLENDER BODIES OF REVOLUTIONJUNGER MC.1982; JOURNAL OF THE ACOUSTICAL SOCIETY OF AMERICA; ISSN 0001-4966; USA; DA. 1982; VOL. 72; NO 6; PP. 1954-1956; BIBL. 7 REF.Article

INFLUENCE DE LA ROTATION SUR LES CARACTERISTIQUES AERODYNAMIQUES DE CORPS AXISYMETRIQUES, DE GRAND ALLONGEMENT, A DES VITESSES SUPERSONIQUESBYCHKOV NM; ISHTULOV AG; KOVALENKO VM et al.1981; IZV. SIB. OTD. AKAD. NAUK SSSR, SER. TEH. NAUK; ISSN 0002-3434; SUN; DA. 1981; NO 3; PP. 65-74; BIBL. 11 REF.Article

MAGNETOHYDRODYNAMICAL UNSTEADY FLOW PAST A SLENDER BODY OF AN ARBITRARY CROSS-SECTION.SUWA S; KUSUKAWA K.1974; J. PHYS. SOC. JAP.; JAP.; DA. 1974; VOL. 36; NO 4; PP. 1174-1184; BIBL. 15 REF.Article

ERWEITERUNG DER PARABOLISCHEN METHODE FUER SCHALLNAHE STROEMUNGEN: INSTATIONAERE STROEMUNG. = EXTENSION DE LA METHODE PARABOLIQUE POUR DES ECOULEMENTS TRANSSONIQUES: ECOULEMENT NON STATIONNAIREOEHMEN KH; TEIPEL I.1975; Z. ANGEW. MATH. MECH.; DTSCH.; DA. 1975; VOL. 55; NO 4; PP. 145-146; BIBL. 4 REF.; (WISS. JAHRESTAG. GES. ANGEW. MATH. MECH. VORTR.; BOCHUM; 1974)Conference Paper

AXISYMMETRIC SONIC FLOW COMPUTED BY A NUMERICAL METHOD APPLIED TO SLENDER BODIES.SEDIN YCJ.1975; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 4; PP. 504-511; BIBL. 19 REF.Article

EVALUATION OF DRAG INTEGRAL USING CUBIC SPLINES.JAMES RM; PANICO VD.1974; J. AIRCR.; U.S.A.; DA. 1974; VOL. 11; NO 8; PP. 494-496; BIBL. 4 REF.Article

HYDRODYNAMIC FORCES CAUSED BY SHIP IN CONFINED WATERSBECK RF.1981; PROC. AM. SOC. DIV. ENG., J. ENG. MECH. DIV.; ISSN 0044-7951; USA; DA. 1981; VOL. 107; NO 3; PP. 523-546; BIBL. 39 REF.Article

INDUCED DRAG OF A SLENDER WING IN A NONUNIFORM STREAMHANIN M; BARSONY NACY A.1983; AIAA JOURNAL; ISSN 0001-1452; USA; DA. 1983; VOL. 21; NO 5; PP. 781-783; BIBL. 4 REF.Article

CANCELLATION EFFECT AND PARAMETER IDENTIFIABILITY OF SHIP STEERING DYNAMICSWEI YUAN HWANG.1982; INT. SHIPBUILD. PROG.; ISSN 0020-868X; NLD; DA. 1982; VOL. 29; NO 332; PP. 90-102; BIBL. 16 REF.Article

NUMERICAL INVESTIGATION OF FLOWFIELD ABOUT A SERIES OF INDENTED NOSETIPSHSIEH T.1981; AEROSPACE SCIENCES MEETING. 19 /1981-01-12/SAINT LOUIS MO; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1981; 10 P.; H.T. 1; BIBL. 16 REF.Conference Paper

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