共 50 条
- [31] AN IMPROVED UPWIND FINITE VOLUME RELAXATION METHOD FOR HIGH-SPEED VISCOUS FLOWSJOURNAL OF COMPUTATIONAL PHYSICS, 1992, 99 (01) : 159 - 168TAYLOR, ACNG, WFWALTERS, RW
- [33] Numerical prediction of film cooling effectiveness over flat plate using variable turbulent prandtl number closuresJournal of Thermal Science, 2016, 25 : 280 - 286Tomasz Ochrymiuk
- [34] A NOTE ON HYPERSONIC VISCOUS FLOW OVER A FLAT PLATEJOURNAL OF THE AERONAUTICAL SCIENCES, 1953, 20 (07): : 502 - 504PAI, SI
- [35] The effects of Prandtl number on black hole accretion flowsNEW ASTRONOMY REVIEWS, 2008, 51 (10-12) : 814 - 818Balbus, Steven A.Lesaffre, Pierre
- [36] Scale effects of incipient cavitation for high-speed flowsPROCEEDINGS OF THE INSTITUTION OF CIVIL ENGINEERS-WATER MANAGEMENT, 2013, 166 (07) : 402 - 408Zhang, Jian-MinWang, Yu-RongYang, QingXu, Wei-Lin
- [37] An Analytical Solution for Boundary Layer Flows Over a Moving-Flat Porous Plate With Viscous DissipationJOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME, 2014, 136 (02):Toki, C. J.
- [38] Acoustic receptivity of high-speed boundary layers on a flat plate at angles of attackTHEORETICAL AND COMPUTATIONAL FLUID DYNAMICS, 2022, 36 (05) : 705 - 722Fedorov, Alexander, VPalchekovskaya, Natalia
- [39] Acoustic receptivity of high-speed boundary layers on a flat plate at angles of attackTheoretical and Computational Fluid Dynamics, 2022, 36 : 705 - 722Alexander V. FedorovNatalia Palchekovskaya
- [40] WALL TEMPERATURE AND PRANDTL NUMBER EFFECTS ON TURBULENT BOUNDARY LAYER THICKNESSES AND SHAPE FACTORS FOR SUBSONIC COMPRESSIBLE GAS FLOW OVER A FLAT PLATEJOURNAL OF ENGINEERING FOR POWER, 1969, 91 (04): : 281 - &KELNHOFE.WJ