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INVISCID-VISCOUS INTERACTIONS IN THE NEARLY DIRECT DESIGN OF SHOCK-FREE SUPERCRITICAL AIRFOILSNEBECK HE; SEEBASS AR; SOBIECZKY H et al.1981; AGARD CONF. PROC.; ISSN 0549-7191; FRA; DA. 1981; NO 291; PP. 3.1-3.10; BIBL. 21 REF.Article

LAMINAR VISCOUS-INVISCID INTERACTIONS AT TRANSONIC SPEEDS.COLLINS DJ.1974; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1974; VOL. 12; NO 8; PP. 1146-1149; BIBL. 7 REF.Article

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

A DIRECT-INVERSE TECHNIQUE FOR LOW SPEED HIGH LIFT AIRFOIL FLOWFIELD ANALYSISCARLSON LA.1981; AGARD CONF. PROC.; ISSN 0549-7191; FRA; DA. 1981; NO 291; PP. 26.1-26.10; BIBL. 18 REF.Article

ANALYTICAL PROCEDURE FOR CALCULATION OF ATTACHED AND SEPARATED SUBSONIC DIFFUSER FLOWS.BOWER WW.1976; J. AIRCR.; U.S.A.; DA. 1976; VOL. 13; NO 1; PP. 49-56; BIBL. 11 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

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

CALCULATIONS OF TRANSONIC FLOW OVER WING/BODY COMBINATIONS WITH AN ALLOWANCE FOR VISCOUS EFFECTSFIRMIN MCP.1981; AGARD CONF. PROC.; ISSN 0549-7191; FRA; DA. 1981; NO 291; PP. 8.1-8.18; BIBL. 21 REF.Article

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

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

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

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

Spanwise propagation of upstream influence in conical swept shock/boundary-layer interactionsINGER, G. R.AIAA journal. 1987, Vol 25, Num 2, pp 287-293, issn 0001-1452Article

Calculation of the mean flow past circular cylinders by viscous-inviscid interactionCELIK, I; PATEL, V. C; LANDWEBER, L et al.Journal of fluids engineering. 1985, Vol 107, Num 2, pp 218-223, issn 0098-2202Article

The prediction of separated flow using a viscous-inviscid interaction methodWILLIAMS, B. R.Aeronautical Journal. 1985, Vol 89, Num 885, pp 185-197, issn 0001-9240Article

A new technique for computing viscous-inviscid interactions in internal flowsSTRAWN, R. C; FERZIGER, J. H; KLINE, S. J et al.Journal of fluids engineering. 1984, Vol 106, Num 1, pp 79-84, issn 0098-2202Article

Viscous-inviscid interactive procedure for rotational flow in cascades of airfoilsJOHNSTON, W; SOCKOL, P.AIAA journal. 1984, Vol 22, Num 9, pp 1281-1282, issn 0001-1452Article

Airfoils with separation and the resulting wakesCEBECI, T; CLARK, R. W; CHANG, K. C et al.Journal of Fluid Mechanics. 1986, Vol 163, pp 323-347, issn 0022-1120Article

Developments in computational methods for hight-lift aerodynamicsKING, D. A; WILLIAMS, B. R.Aeronautical Journal. 1988, Vol 92, Num 917, pp 265-288, issn 0001-9240Article

VISCOUS-INVISCID INTERACTION ON OSCILLATING AIRFOILS IN SUBSONIC FLOWMCCROSKEY WJ; PUCCI SL.1982; AIAA J.; ISSN 0001-1452; USA; DA. 1982; VOL. 20; NO 2; PP. 167-174; BIBL. 10 REF.Article

ANALYSIS OF SEPARATED BOUNDARY-LASER FLOWSCARTER JE; VATSA VN.1982; LECT. NOTES PHYS.; ISSN 0075-8450; DEU; DA. 1982; VOL. 170; PP. 167-174; BIBL. 15 REF.Conference Paper

ANALYSIS OF STALLED AIRFOILS BY SIMULTANEOUS PERTURBATIONS TO VISCOUS AND INVISCID EQUATIONSGILMER BR; BRISTOW DR.1982; AIAA J.; ISSN 0001-1452; USA; DA. 1982; VOL. 20; NO 9; PP. 1160-1166; BIBL. 10 REF.Article

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

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

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