Microramp Control of Supersonic Oblique Shock-Wave/Boundary-Layer Interactions
Microramp Control of Supersonic Oblique Shock-Wave-Boundary-Layer Interactions
ERRATA - Effect of Surface Roughness on Unseparated Shock-Wave-Turbulent Boundary-Layer Interactions
INTERDISCIPLINARY TOPICS - Geometries for Five-Hole-Type Probes with Planar Sensor Arrays (TN)
Shock-Wave/Boundary-Layer Interaction Control Using Three-Dimensional Bumps for Transonic Wings
Shock-Wave-Boundary-Layer Interaction Control Using Three-Dimensional Bumps for Transonic Wings
Vortical Structures on Three-Dimensional Shock Control Bumps
Vortical Structures on Three-Dimensional Shock Control Bumps
Vortical Structures on Three-Dimensional Shock Control Bumps
Joint Experimental and Numerical Approach to Three-Dimensional Shock Control Bump Research
Joint Experimental and Numerical Approach to Three-Dimensional Shock Control Bump Research
Low Reynolds Number Experimental Studies on Flat Plates (AIAA 2014-0743)
An Investigation of Interactions between Normal Shocks and Transitional Boundary Layers
2012-2812 Comparison of Micro-Vortex Generators in Supersonic Flows
Flow Physics of a Normal-hole Bled Supersonic Turbulent Boundary Layer
Experimental and Computational Investigations of a Normal-Hole-Bled Supersonic Boundary Layer
Experimental and Computational Investigations of a Normal-Hole-Bled Supersonic Boundary Layer
AN EXPERIMENTAL STUDY INTO THE FLOW PHYSICS OF THREE-DIMENSIONAL SHOCK CONTROL BUMPS
CHARACTERIZATION OF MICRO-VORTEX GENERATORS IN SUPERSONIC FLOWS
LEADING EDGE VORTEX DEVELOPMENT ON A WAVING WING AT REYNOLDS NUMBERS BETWEEN 10,000 AND 60,000
Corner Effect and Asymmetry in Transonic Channel Flows
Corner Effect and Asymmetry in Transonic Channel Flows
LOW REYNOLDS NUMBER EXPERIMENTS ON AN IMPULSIVELY STARTED FLAT PLATE AT HIGH INCIDENCE
MICRO-VORTEX GENERATORS APPLIED TO A FLOW-FIELD CONTAINING A NORMAL SHOCK-WAVE AND DIFFUSER
Behaviour of Unsteady Transonic Shock/Boundary Layer Interactions with Three-Dimensional Effects
Quantitative Heat Transfer Measurement using Liquid Crystal Thermography in an Hypersonic Gun Tunnel
A Representative Flowfield of External Compression Inlets and Diffusers
The Effect of Tunnel Size on Incident Shock Boundary Layer Interaction Experiments