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TRANSONIC LAMINAR VISCOUS-INVISCID INTERACTION OVER AIRFOILS.TAI TC.1975; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 8; PP. 1065-1072; BIBL. 29 REF.Article

EXTENSION OF THE MOMENTUM INTEGRAL METHOD TO THREE-DIMENSIONAL VISCOUS-INVISCID INTERACTIONS.GEORGEFF MP.1974; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1974; VOL. 12; NO 11; PP. 1603-1605; BIBL. 6 REF.Article

A REVIEW OF METHODS FOR PREDICTING VISCOUS EFFECTS ON AEROFOILS AND WINGS AT TRANSONIC SPEEDSLOCK RC.1981; AGARD CONF. PROC.; ISSN 0549-7191; FRA; DA. 1981; NO 291; PP. 2.1-2.32; BIBL. 62 REF.Article

AN ANALYTICAL METHOD TO COMPUTE VISCOUS-INVISCID TRANSONIC FLOW ON AXISYMMETRIC AFTERBODIES INCLUDING JET EFFECTS AND BOATTAIL BLEED IN SEPARATED REGIONS.CALARESE W.1975; IN: AM. INST. AERONAUT. ASTRONAUT.-SOC. AUTOMOT. ENG. PROPUL. CONF. 11; ANAHEIM, CALIF.; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 1293; PP. 1-9; BIBL. 18 REF.Conference Paper

TRANSONIC LAMINAR VISCOUS-INVISCID INTERACTION OVER AIRFOILS.TAI TC.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 7TH FLUID PLASMA DYN. CONF.; PALO ALTO, CALIF.; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 600; PP. 1-11; BIBL. 29 REF.Conference Paper

THE ANALYSIS OF FLOW FLIELDS WITH SEPARATION BY NUMERICAL MATCHING. = ANALYSE DES CHAMPS D'ECOULEMENT AVEC DECOLLEMENT PAR RACCORDEMENT NUMERIQUEBRUNE GW; RUBBERT PE; FORESTER CK et al.1975; A.G.A.R.D. CONF. PROC.; FR.; DA. 1975; NO 168; PP. 16.1-16.8; BIBL. 6 REF.; (FLOW SEP. FLUID DYN. PANEL SYMP.; GOETTINGEN, GER.; 1975)Conference Paper

MOMENTUM INTEGRAL METHOD FOR VISCOUS-INVISCID INTERACTIONS WITH ARBITRARY WALL COOLING.GEORGEFF MP.1974; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1974; VOL. 12; NO 10; PP. 1393-1400; BIBL. 33 REF.Article

EXTERNAL FLOWS.FERNHOLZ HH.1976; TOPICS APPL. PHYS.; GERM.; DA. 1976; VOL. 12; PP. 45-107; BIBL. 10 P.Article

SUPERCRITICAL TRANSONIC TRAILING-EDGE FLOWBODONYI RJ; KLUWICK A.1982; Q.J. MECH. APPL. MATH.; ISSN 0033-5614; GBR; DA. 1982; VOL. 35; NO 2; PP. 265-277; BIBL. 12 REF.Article

TURBULENT INTERACTIONS ON AIRFOILS AT TRANSONIC SPEEDS: RECENT DEVELOPMENTSMELNIK RE.1981; AGARD CONF. PROC.; ISSN 0549-7191; FRA; DA. 1981; NO 291; PP. 10.1-10.34; BIBL. 74 REF.Article

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

VISCID-INVISCID INTERACTION OF INCOMPRESSIBLE SEPARATED FLOWS.CHOW WL; SPRING DJ.1976; J. APPL. MECH.; U.S.A.; DA. 1976; VOL. 43; NO 3; PP. 387-395; BIBL. 15 REF.Article

AN EXPERIMENTAL INVESTIGATION OF TURBULENT TRANSONIC VISCOUS-INVISCID INTERACTIONSALBER IE; BACON JW; MASSON BS et al.1973; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1973; VOL. 11; NO 5; PP. 620-627; BIBL. 20 REF.Serial Issue

THE COUPLING OF A SHOCK BOUNDARY LAYER INTERACTION MODULE WITH A VISCOUS-INVISCID COMPUTATION METHODSTANEWSKY E; NANDANAN M; INGER GR et al.1981; AGARD CONF. PROC.; ISSN 0549-7191; FRA; DA. 1981; NO 291; PP. 4.1-4.14; BIBL. 22 REF.Article

COMPUTATION OF VISCOUS-INVISCID INTERACTIONS = LE CALCUL DE L'INTERACTION FLUIDE PARFAIT-FLUIDE VISQUEUXLE BALLEUR JC.1981; ; FRA; NEUILLY-SUR-SEINE: AGARD; DA. 1981; AGARD/AR-171; 15 P.; 30 CM; BIBL. 2 P.; 92-835-0300-7Report

VISCOUS-INVISCID INTERACTION ON OSCILLATING AIRFOILS IN SUBSONIC FLOWMCCROSKEY WJ; PUCCI SL.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. 11 REF.Conference Paper

VISCOUS-INVISCID INTERACTION FOR TRANSONIC WING-BODY CONFIGURATIONS INCLUDING WAKE EFFECTSSTREET CL.1982; AIAA J.; ISSN 0001-1452; USA; DA. 1982; VOL. 20; NO 7; PP. 915-923; BIBL. 22 REF.Article

PLANAR TRANSONIC AIRFOIL COMPUTATIONS WITH VISCOUS INTERACTIONSWAI JC; YOSHIHARA H.1981; AGARD CONF. PROC.; ISSN 0549-7191; FRA; DA. 1981; NO 291; PP. 9.1-9.9; BIBL. 9 REF.Article

TRANSONIC VISCOUS-INVISCID INTERACTION OVER AIRFOILS FOR SEPARATED LAMINAR OR TURBULENT FLOWSGORDON R; ROM J.1981; AIAA J.; ISSN 0001-1452; USA; DA. 1981; VOL. 19; NO 5; PP. 545-552; BIBL. 26 REF.Article

ANALYSIS OF LEADING-EDGE SEPARATION BUBBLES OF AIRFOILS.CRIMI P; REEVES BL.1976; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1976; VOL. 14; NO 11; PP. 1548-1555; BIBL. 18 REF.Article

SUPERSONIC LAMINAR FLOW PAST A SMALL REAR-FACING STEP.INGER GR.1974; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1974; VOL. 12; NO 6; PP. 739-740; BIBL. 2 REF.Article

BERECHNUNG EBENER DIFFUSOREN = CALCUL DES DIFFUSEURS PLANSGERSTEN K; HERWIG H; SCHMIDT G et al.1983; ZEITSCHRIFT FUER FLUGWISSENSCHAFTEN UND WELTRAUMFORSCHUNG; ISSN 0342-068X; DEU; DA. 1983; VOL. 7; NO 3; PP. 183-192; ABS. ENG; BIBL. 10 REF.Article

THE CALCULATION OF INCOMPRESSIBLE BOUNDARY LAYERS WITH STRONG VISCOUS-INVISCID INTERACTIONVELDMAN AEP.1981; AGARD CONF. PROC.; ISSN 0549-7191; FRA; DA. 1981; NO 291; PP. 12.1-12.12; BIBL. 31 REF.Article

TOWARD A SPLINE TECHNIQUE FOR THE HIGH REYNOLDS NUMBER INTERACTION (TRIPLE DECK) PROBLEMNAPOLITANO M; VACCA G.1981; AGARD CONF. PROC.; ISSN 0549-7191; FRA; DA. 1981; NO 291; PP. 29.1-29.15; BIBL. 32 REF.Article

AXISYMMETRIC TRANSONIC TURBULENT BASE PRESSURESLIU JSK; CHOW WL.1979; A.I.A.A.J., NEW YORK; USA; DA. 1979; VOL. 17; NO 4; PP. 330-331; BIBL. 9 REF.Article

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