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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

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

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

COMPUTATIONAL STUDY OF THE MAGNUS EFFECT ON BOATTAILED SHELLSTUREK WB; MYLIN DC.1982; AIAA J.; ISSN 0001-1452; USA; DA. 1982; VOL. 20; NO 10; PP. 1462-1464; BIBL. 5 REF.Article

SUR LA REGULARITE DE LA FONCTION DE GREEN DU PROBLEME DE NEUMANN-KELVINEUVRARD D.1982; REV. ROUM. MATH. PURES APPL.; ISSN 0035-3965; ROM; DA. 1982; VOL. 27; NO 3; PP. 319-326; BIBL. 13 REF.Article

NAVIER-STOKES SOLUTION OF A SLENDER BODY OF REVOLUTION AT LARGE INCIDENCEHANKEY WL; GRAHAM JE; SHANG JS et al.1981; AEROSPACE SCIENCES MEETING. 19 /1981-01-12/SAINT LOUIS MO; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1981; 8 P.; BIBL. 15 REF.Conference Paper

THE EFFECT OF ROLL ANGLE ON THE FLOW OVER A SLENDER BODY OF REVOLUTION AT HIGH ANGLES OF ATTACKDEXTER PC; HUNT BL.1981; AEROSPACE SCIENCES MEETING. 19 /1981-01-12/SAINT LOUIS MO; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1981; 13 P.; BIBL. 18 REF.Conference Paper

VORTEX DEVELOPMENT ON SLEUDER MISSILES AT SUPERSONIC SPEEDSALLEN JM; DILLENIUS MFE.1980; J. SPACECR. ROCK.; USA; DA. 1980; VOL. 17; NO 4; PP. 377-378; BIBL. 1 REF.Article

HYPERSONIC SLENDER-WEDGE ANALYSIS WITH GRADUAL CHANGE IN ANGLE OF ATTACKGUPTA RN; JOSHI SP; RODKIEWICZ CM et al.1983; ACTA MECHANICA; ISSN 0001-5970; AUT; DA. 1983; VOL. 47; NO 1-2; PP. 107-115; BIBL. 7 REF.Article

LE PROBLEME DU RAYONNEMENT DES BATEAUX MINCES AVEC UNE VITESSE D'AVANCEMENTMATSUNAGA K; MARUO H.1981; J. SOC. NAV. ARCHIT. JPN.; ISSN 0514-8499; JPN; DA. 1981-12; VOL. 150; PP. 190-200; ABS. ENG; BIBL. 18 REF.Article

AN EXPERIMENTAL STUDY OF VORTEX FLOW IN THE WAKE OF A SLENDER BODY OF REVOLUTION AT LARGE INCIDENCECALARESE W.1981; AEROSPACE SCIENCES MEETING. 19 /1981-01-12/SAINT LOUIS MO; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1981; 8 P.; BIBL. 13 REF.Conference Paper

OPTIMIERUNG DES RELAXATIONSWIDERSTANDS SCHLANKER PROFIL-ANORDNUNGEN IN STATIONAERER UNTERSCHALLSTROEMUNG. I: EINZELPROFIL = OPTIMISATION DE LA TRAINEE DE RELAXATION D'ARRANGEMENTS DE PROFILS ELANCES DANS UN ECOULEMENT SUBSONIQUE STATIONNAIRE I: PROFIL UNIQUESCHILLING H.1980; Z. FLUGWISSENSCH. WELTR.-FORSCH.; DEU; DA. 1980; VOL. 4; NO 3; PP. 148-157; ABS. ENG; BIBL. 17 REF.Article

FINITE DIFFERENCE COMPUTATION OF PRESSURE AND WAVE-DRAG OF SLENDER BODIES OF REVOLUTION AT TRANSONIC SPEEDS WITH ZERO-LIFTLI SHOU YING; LUO SHI JUN.1982; LECT. NOTES PHYS.; ISSN 0075-8450; DEU; DA. 1982; VOL. 170; PP. 350-356; BIBL. 7 REF.Conference Paper

HYPERSONIC FLOW PAST AN AXISYMMETRIC BODY WITH SMALL LONGITUDINAL CURVATUREJISCHKE MC; KIM BS.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. 11 REF.Conference Paper

SLENDER WING THEORY FOR NONUNIFORM STREAMHANIN M; BARSONY NAGY A.1980; AIAA J.; ISSN 0001-1452; USA; DA. 1980; VOL. 18; NO 4; PP. 381-384; BIBL. 8 REF.Article

VORTEX-INDUCED OSCILLATION OF BLUFF CYLINDERSKOMATSU S; KOBAYASHI H.1980; J. WIND ENG. IND. AERODYN.; NLD; DA. 1980; VOL. 6; NO 3-4; PP. 335-362; BIBL. 12 REF.Article

EXPERIMENTAL AND NUMERICAL RESULTS OF SOUND SCATTERING BY A BODYMAESTRELLO L; BAYLISS A.1979; SPECIAL COURSE ON ACOUSTIC WAVE PROPAGATION; FRA; DA. 1979; AGARD-R686; PP. 15.1-15.12; BIBL. 9 REF.Conference Paper

MOTION OF A SLENDER BODY IN STILL POLYMER SOLUTIONHORIKAWA A; CHIBA K.1982; TECHNOLOGY REPORTS OF THE OSAKA UNIVERSITY; ISSN 0030-6177; JPN; DA. 1982; VOL. 32; NO 1652-1683; PP. 373-380; BIBL. 3 REF.Article

ON THE ANALYSIS OF TURBULENT BOUNDARY LAYERS ON SLENDER CYLINDERSACKROYD JAD.1982; J. FLUIDS ENG.; ISSN 0098-2202; USA; DA. 1982; VOL. 104; NO 2; PP. 185-190; BIBL. 13 REF.Article

L'ETUDE DE L'ECOULEMENT SUPERSONIQUE SUR LES CORPS ELANCES EMOUSSES DE SECTION TRANSVERSALE ELLIPTIQUEANTONETS AV; LIPNITSKIJ YU M.1976; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1976; NO 6; PP. 155-159; BIBL. 12 REF.Article

THE MENISCUS ON A NEEDLE - A LESSON IN MATCHINGLO LL.1983; JOURNAL OF FLUID MECHANICS; ISSN 0022-1120; GBR; DA. 1983; VOL. 132; PP. 65-78; BIBL. 11 REF.Article

KRITISCHER ANSTELLWINKEL BEI DER UMSTROEMUNG VON ROTATIONSELLIPSOIDEN = ANGLE D'INCIDENCE CRITIQUE POUR L'ECOULEMENT AUTOUR D'ELLIPSOIDES DE REVOLUTIONGRUNDMANN R.1982; Z. FLUGWISS. WELTRAUMFORSCH.; ISSN 0342-068X; DEU; DA. 1982; VOL. 6; NO 6; PP. 441-442; ABS. ENG; BIBL. 2 REF.Article

MEASUREMENTS OF SURFACE ROUGHNESS EFFECTS ON THE HEAT TRANSFER SLENDER CONES AT MACH 10HILL JAF; VOISINET RLP; WAGNER DA et al.1980; AEROSPACE SCIENCES MEETING. 18/1980/PASADENA CA; USA; NEW YORK: AIAA; DA. 1980; 15 P.; BIBL. 18 REF.Conference Paper

FLAT SPIN OF SLENDER BODIES AT HIGH ANGLES OF ATTACKKUBOTA H; ARAI I; MATSUZAKA M et al.1983; JOURNAL OF SPACECRAFT AND ROCKETS; ISSN 0022-4650; USA; DA. 1983; VOL. 20; NO 2; PP. 108-114; BIBL. 16 REF.Conference Paper

ON THE MOTION OF A SLENDER BODY NEAR AN INTERFACE BETWEEN TWO IMMISCIBLE LIQUIDS AT VERY LOW REYNOLDS NUMBERSFULFORD GR; BLAKE JR.1983; JOURNAL OF FLUID MECHANICS; ISSN 0022-1120; GBR; DA. 1983; VOL. 127; PP. 203-217; BIBL. 2 P.Article

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