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ANSTRICHMITTEL
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Attenuation of Flow Separation Using Herringbone Riblets at
Using Pressure- and Temperature-Sensitive Paint on the Aftbody of a Capsule Entry Vehicle
Full-Field Uncertainty Determination for Pressure-Sensitive Paint Measurements
Full-Field Pressure and Strain Measurement Technique Using a Dual-Layer Luminescent Coating
Development of Sprayable Pressure-Sensitive Paint with a Response Time of Less Than
Characterization of Frequency Response of Pressure-Sensitive Paints
Frequency-Response Characteristics of Polymer/Ceramic Pressure-Sensitive Paint
Numerical and Experimental Studies of Transpiration Cooling Film Effectiveness over Porous Materials
Boundary Layer Transition Preflight Experiments in a Mach-6 Quiet Tunnel
Upstream Vortex Effects on Turbine Blade Platform Film Cooling With Typical Purge Flow
Low-Reynolds-Number Flowfield of Wing with Control Surface in Propeller Slipstream
Film-Cooling Effectiveness of Antivortex Holes at Three Different Mainstream Turbulence Levels
Aerodynamic Data Fusion Toward the Digital Twin Paradigm
Introduction: Advanced Measurement Techniques in Aerospace
Simplified Measurement Method of Oscillating Liquid-Jet Frequency Through Laser Detection