PROGRES RECENTS DANS LES ETUDES EXPERIMENTALES D'ARRIERE-CORPS.MECHIN B.1975; AERONAUT. ET ASTRONAUT.; FR.; DA. 1975; NO 50; PP. 27-33; ABS. ANGL. ALLEM.; BIBL. 7 REF.Article

COUPLAGE ENTRE L'ECOULEMENT AUTOUR D'UN ARRIERE-CORPS ET LE JET PROPULSIF EN THEORIE DE FLUIDE PARFAIT.MARIA SUBE R; CHATTOT JJ; GILLON G et al.1974; CHATILLON; OFF. NATL. ETUD. RECH. AEROSP.; DA. 1974; PP. 1-12; ABS. ANGL.; BIBL. 14 REF.; (REUN. AGARD INTERFERENCE ENTRE CELL. PROPUL.; ROME; 1974)Conference Paper

IMPROVED INTERACTION METHOD FOR EXHAUST NOZZLE BOATTAIL FLOWSKUHN GD.1981; AIAA J.; ISSN 0001-1452; USA; DA. 1981; VOL. 19; NO 3; PP. 358-359; BIBL. 6 REF.Article

A COMPARISON OF JET TEMPERATURE EFFECTS ON AFTERBODY DRAG WITH THOSE FROM JET MOLECULAR WEIGHT AND NOZZLE AREA RATIO VARIATIONSPETERS WL.sdJOINT PROPULSION CONFERENCE. 16/1980/HARTFORD CT; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. S.D.; 11 P.; BIBL. 7 REF.Conference Paper

FINITE ELEMENT ANALYSIS OF INVISCID SUBSONIC BOATTAIL FLOWCHIMA RV; GERHART PM.1981; AEROSPACE SCIENCES MEETING. 19 /1981-01-12/SAINT LOUIS MO; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1981; 16 P.; BIBL. 32 REF.Conference Paper

A VISCOUS-INVISCID INTERACTION MODEL OF JET ENTRAINMENTVILMOTH RG; DASH SM.1981; AGARD CONF. PROC.; ISSN 0549-7191; FRA; DA. 1981; NO 291; PP. 13.1-13.15; BIBL. 18 REF.Article

AN IMPROVED INTERACTION METHOD FOR EXHAUST NOZZLE BOATTAIL FLOWKUHN GD.1980; AEROSPACE SCIENCES MEETING. 18/1980/PASADENA CA; USA; NEW YORK: AIAA; DA. 1980; 9 P.; BIBL. 13 REF.Conference Paper

NUMERICAL SIMULATION OF THREE-DIMENSIONAL BOATTAIL AFTERBODY FLOWFIELDSDEIWERT GS.1981; AIAA J.; ISSN 0001-1452; USA; DA. 1981; VOL. 12; NO 5; PP. 582-588; BIBL. 15 REF.Article

EXPERIMENTAL INVESTIGATION OF FLOW SEPARATION ON AFTERBODIES WITH A CENTERED PROPULSIVE JET AND SUPERSONIC EXTERNAL FLOW AT SMALL ANGLES OF ATTACKAGRELL J.1979; JB. DTSCH. GESELLSCH. LUFT-U. RAUMFAHRT; DEU; DA. 1979 PUBL. 1980; PP. 9Article

COMPUTATIONAL OF A SUPERSONIC FLOW PAST AN AXISYMMETRIC NOZZLE BOATTAIL WITH JET EXHAUSTMIKHAIL AG; HANKEY WL; SHANG JS et al.1980; AIAA J.; ISSN 0001-1452; USA; DA. 1980; VOL. 18; NO 8; PP. 869-875; BIBL. 23 REF.Article

THE SIMULATION AND MODELING OF JET PLUMES IN WIND TUNNEL FACILITIESKORST HH; WHITE RA; NYBERG SE et al.1980; AERODYNAMICS TESTING CONFERENCE. 11/1980/COLORADO SPRINGS CO; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1980; PP. 104-116; BIBL. 20 REF.Conference Paper

FAST NAVIER-STOKES SOLUTION OF TRANSONIC FLOWFIELD ABOUT AXISYMMETRIC AFTERBODIESCOSNER RR.1980; AEROSPACE SCIENCES MEETING. 18/1980/PASADENA CA; USA; NEW YORK: AIAA; DA. 1980; 8 P.; BIBL. 14 REF.Conference Paper

NUMERICAL SIMULATION OF STEADY SUPERSONIC FLOW OVER AN OGIVE-CYLINDER-BOATTAIL BODYSCHIFF LB; STUREK WB.1980; AEROSPACE SCIENCES MEETING. 18/1980/PASADENA CA; USA; NEW YORK: AIAA; DA. 1980; 11 P.; BIBL. 14 REF.Conference Paper

ETUDE EXPERIMENTALE DU DECOLLEMENT AU BORD DE FUITE D'UN ARRIERE-CORPS DE REVOLUTION PROFILESOLIGNAC JL.1980; RECH. AEROSP.; ISSN 0034-1223; FRA; DA. 1980; NO 3; PP. 205-211; ABS. ENG; BIBL. 4 REF.Article

Calcul des caractéristiques des écoulements lors de l'insufflation uniforme d'un gaz homogène dans la partie arrière d'un corpsBELOTSERKOVETS, I. S; TIMOSHENKO, V. I.Prikladnaâ mehanika i tehničeskaâ fizika. 1984, Num 1, pp 76-81, issn 0869-5032Article

A MODIFIED DISPLACEMENT-BODY METHOD FOR TREATING THE AXISYMMETRIC STRONG-INTERACTION PROBLEMHOFFMAN GH.1980; J. SHIP RES.; USA; DA. 1980; VOL. 24; NO 2; PP. 114-122; BIBL. 21 REF.Article