Citation: N. Okongo et Dd. Knight, IMPLICIT UNSTRUCTURED NAVIER-STOKES SIMULATION OF LEADING-EDGE SEPARATION OVER A PITCHING AIRFOIL, Applied numerical mathematics, 27(3), 1998, pp. 269-308
Citation: G. Scharnhorst et Dd. Knight, GILMAN,CHARLOTTE,PERKINS LIBRARY - A RECONSTRUCTION (BIBLIOGRAPHY), Resources for American literary study, 23(2), 1997, pp. 181-219
Citation: Pg. Choudhuri et Dd. Knight, EFFECTS OF COMPRESSIBILITY, PITCH RATE, AND REYNOLDS-NUMBER ON UNSTEADY INCIPIENT LEADING-EDGE BOUNDARY-LAYER SEPARATION OVER A PITCHING AIRFOIL, Journal of Fluid Mechanics, 308, 1996, pp. 195-217
Authors:
GARRISON TJ
SETTLES GS
NARAYANSWAMI N
KNIGHT DD
HORSTMAN CC
Citation: Tj. Garrison et al., FLOWFIELD SURVEYS AND COMPUTATIONS OF A CROSSING-SHOCK WAVE BOUNDARY-LAYER INTERACTION, AIAA journal, 34(1), 1996, pp. 50-56
Citation: A. Cui et Dd. Knight, PARALLEL COMPUTATION OF THE 2-D NAVIER-STOKES FLOWFIELD OF A PITCHINGAIRFOIL, International journal of computational fluid dynamics, 4(1-2), 1995, pp. 111-135
Citation: Dd. Knight, A FULLY IMPLICIT NAVIER-STOKES ALGORITHM USING AN UNSTRUCTURED GRID AND FLUX-DIFFERENCE SPLITTING, Applied numerical mathematics, 16(1-2), 1994, pp. 101-128
Authors:
GARRISON TJ
SETTLES GS
NARAYANSWAMI N
KNIGHT DD
Citation: Tj. Garrison et al., LASER INTERFEROMETER SKIN-FRICTION MEASUREMENTS OF CROSSING-SHOCK-WAVE TURBULENT-BOUNDARY-LAYER INTERACTIONS, AIAA journal, 32(6), 1994, pp. 1234-1241
Citation: Dd. Knight, WITH-THE-1ST-GRASS-BLADE - WHITMAN INFLUENCE ON THE POETRY OF GILMAN,CHARLOTTE,PERKINS, Walt Whitman quarterly review, 11(1), 1993, pp. 18-29
Citation: N. Narayanswami et al., COMPUTATION OF CROSSING SHOCK TURBULENT BOUNDARY-LAYER INTERACTION ATMACH-8.3, AIAA journal, 31(8), 1993, pp. 1369-1376