Laminar boundary layer separation at a fin-body junction in a hypersonic flow," Shock wave, vol. 11, no. 1, pp. 31-42, 2001. J.D. Smith and V. Sick, "Crank-angle resolved imaging of biacetyl laser-A.F.P. Houwing,, D.R. Smith, J.S. Fox, P.M. Danehy, N.R. Mud- ford...
Shock wave boundary layer interactions in hypersonic flowsShock boundary layer interactionHypersonicsSeparationLaminar hypersonic flowShock-wave boundary layer interaction (SWBLI) and associated changes in wall properties for ramp induced flow breakdown have been considered in the present studies. A two ...
Considerable energy is associated with the wake; this energy is taken from the bulk flow. Formation of wakes should be minimised if large pressure losses in the fluid are to be avoided. However, for some purposes such as promotion of mixing and heat transfer, boundary layer separation may be...
Shock-wave=boundary-layer interactions in hypersonic low density ows. AIAA Paper 98-2668, 1998... J Moss 被引量: 0发表: 2004年 A Study of Flow Separation in Regions of Shock Wave-Boundary Layer Interaction in Hypersonic Flow. Holden MS (2014) Experimental studies of shock-wave-boundary- la...
Effects of leading-edge bluntness and ramp deflection angle on laminar boundary-layer separation in hypersonic flow Leading edge bluntness and ramp deflection angle effects on laminar boundary layer separation in hypersonic flow JC Townsend 被引量: 7发表: 1966年 ...
Boundary-layer laminar-turbulent transition effectively affects the aerodynamic lift and drag of hypersonic vehicles and has a great effect on the design of hypersonic vehicles [1-3]. Receptivity of the Boundary Layer over a Blunt Wedge with Distributed Roughness at Mach 6 Then, many similarity sol...
Reduction of shock induced boundary layer separation in hypersonic inlets using bleed inside such a hypersonic inlet is the mutual interaction of oblique shocks with boundary layers, forcing the boundary layer to separate from the inlet wall... HU Wepler - 《Aerospace Science & Technology》 被引量...
HU Meier,HP Kreplin - 《Zeitschrift Für Flugwissenschaften Und Weltraumforschung》 被引量: 103发表: 1980年 Influence of roughness on attachment line boundary layer transition in hypersonic flow ?Attachment line boundary layer transition on swept cylinders is studied in a low enthalpy hypersonic wind...
This entry describes the experimental work conducted in the Department of Aeronautics at Imperial College in connection with Test Problems 1 and 2 of the “Workshop on Hypersonic Flows for Reentry Problems, Part I”. These are defined as follows:...
In the dual-layer block ... S Yamamoto - 《Radiological Physics & Technology》 被引量: 1发表: 2012年 Experimental investigation on aero-heating of rudder shaft within laminar/turbulent hypersonic boundary layers The heat flux on the model surface is measured by thin film heat flux sensors, ...