ON APPLICATION OF BODY CONFORMING CURVILINEAR GRIDS FOR FINITE DIFFERENCE SOLUTION OF EXTERNAL FLOWSTEGER JL.1982; APPL. MATH. COMPUT.; ISSN 0096-3003; USA; DA. 1982; VOL. 10-11; PP. 295-316; BIBL. 18 REF.Conference Paper

COEFFICIENT MATRICES FOR IMPLICIT FINITE DIFFERENCE SOLUTION OF THE INVISCID FLUID CONSERVATION LOW EQUATIONS.STEGER JL.1978; COMPUTER METHODS APPL. MECH. ENGNG; NETHERL.; DA. 1978; VOL. 13; NO 2; PP. 175-188; BIBL. 22 REF.Article

IMPLICIT FINITE-DIFFERENCE SIMULATION OF FLOW ABOUT ARBITRARY TWO-DIMENSIONAL GEOMETRIESSTEGER JL.1978; A.I.A.A. J., NEW YORK; USA; DA. 1978; VOL. 16; NO 7; PP. 679-686; BIBL. 32 REF.Article

FLUX VECTOR SPLITTING OF THE INVISCED GASDYNAMIC EQUATIONS WITH APPLICATION TO FINITE-DIFFERENCE METHODSSTEGER JL; WARMING RF.1981; J. COMPUT. PHYS.; ISSN 0021-9991; USA; DA. 1981; VOL. 40; NO 2; PP. 263-293; BIBL. 32 REF.Article

IMPLICIT FINITE-DIFFERENCE PROCEDURES FOR THE COMPUTATION OF VORTEX WAKES.STEGER JL; KUTLER P.1976; IN: FLUID PLASMA DYN. CONF. 9; SAN DIEGO, CALIF.; 1976; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. 1976; VOL. 385; PP. 1-12; BIBL. 19 REF.Conference Paper

RELAXATION METHODS IN FLUID MECHANICS.LOMAX H; STEGER JL.1975; ANNU. REV. FLUID MECH.; U.S.A.; DA. 1975; VOL. 7; PP. 63-88; BIBL. 1 P. 1/2Article

CALCULATION OF SEPARATED FLOW AT SUBSONIC AND TRANSONIC SPEEDSKLINEBERG JM; STEGER JL.1973; LECTURE NOTES PHYS.; GERM.; DA. 1973; NO 19; PP. 161-168; BIBL. 7 REF.; (PROC. 3RD. INT. CONF. NUMER. METHODS FLUID MECH. II. PROBL. FLUID. MECH.; PARIS; 1972)Conference Paper

NUMERICAL SIMULATION OF STEADY SUPERSONIC VISCOUS FLOWSCHIFF LB; STEGER JL.1980; A.I.A.A. J.; ISSN 0001-1452; USA; DA. 1980; VOL. 18; NO 12; PP. 1421-1430; BIBL. 26 REF.Article

AUTOMATIC MESH-POINT CLUSTERING NEAR A BOUNDARY IN GRID GENERATION WITH ELLIPTIC PARTIAL DIFFERENTIAL EQUATIONSSTEGER JL; SORENSON RL.1979; J. COMPUT. PHYS.; USA; DA. 1979; VOL. 33; NO 3; PP. 405-410; BIBL. 12 REF.Article

ON IMPLICIT FINITE-DIFFERENCE SIMULATIONS OF THREE DIMENSIONAL FLOWPULLIAM TH; STEGER JL.1978; AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS AEROSPACE SCIENCES MEETING. 16/1978/HUNTSVILLE AL; USA; NEW YORK: AIAA; DA. 1978; 78-10; 11 P.; BIBL. 1 P.Conference Paper

A FINITE-DIFFERENCE METHOD FOR TRANSONIC AIRFOIL DESIGNSTEGER JL; KLINEBERG JM.1973; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1973; VOL. 11; NO 5; PP. 628-635; BIBL. 9 REF.Serial Issue

ON LAMINAR BOUNDARY-LAYER SEPARATION.KLINEBERG JM; STEGER JL.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 12TH AEROSP. SCI. MEET.; WASHINGTON; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 94; PP. 1-17; BIBL. 2 P.Conference Paper

RELAXATION TECHNIQUES FOR THREE DIMENSIONAL TRANSONIC FLOW ABOUT WINGSBAILEY FR; STEGER JL.1973; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1973; VOL. 11; NO 3; PP. 318-325; BIBL. 17 REF.Serial Issue

NUMERICAL SOLUTION OF THE AZIMUTHAL-INVARIANT THIN-LAYER NAVIER-STOKES EQUATIONSNIETUBICZ CJ; PULLIAM TH; STEGER JL et al.1980; AIAA J.; ISSN 0001-1452; USA; DA. 1980; VOL. 18; NO 12; PP. 1411-1412; BIBL. 6 REF.Article

A NUMERICAL SIMULATION OF HYPERSONIC VISCOUS FLOW OVER ARBITRARY GEOMETRIES AT HIGH ANGLE OF ATTACKCHAUSSEE DS; PATTERSON JL; KUTLER P et al.1981; AEROSPACE SCIENCES MEETING. 19 /1981-01-12/SAINT LOUIS MO; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1981; 14 P.; BIBL. 25 REF.Conference Paper