Development and Ground Testing of Direct Measuring Skin Friction Gages for High Enthalpy Supersonic Flight Tests.
類似資料:
1
テクニカルペーパー
Development and Ground Testing of Heat Flux Gages for High Enthalpy Supersonic Flight Tests.
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
8
テクニカルペーパー
Directional skin friction measurements in a high enthalpy supersonic flow about a sharp fin
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
10
テクニカルペーパー
In-Flight Capability for Evaluating Skin-Friction Gages and Other Near-Wall Flow Sensors.
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
11
テクニカルペーパー
Direct Skin Friction Measurements with Shock-Impingement Compensation in Complex Turbulent Flows
American Institute of Aeronautics and Astronautics |
6
テクニカルペーパー
Improved Direct Measurement Fiber-Optic Skin Friction Gauge for Flight Test and Laboratory Applications
American Institute of Aeronautics and Astronautics |
12
テクニカルペーパー
Development of Fiber Optic Aerodynamic Sensors for High Reynolds Number Supersonic Flows
American Institute of Aeronautics and Astronautics |