Calibration of the 13- by 13-Inch Adaptive Wall Test Section for the Langley 0.3-Meter Transonic Cryogenic Tunnel
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National Aeronautics and Space Administration |
7
テクニカルペーパー
HIGH REYNOLDS NUMBER TESTS OF A DOUGLAS DLBA 032 AIRFOIL IN THE LANGLEY 0.3-METER TRANSONIC CRYOGENIC TUNNEL
National Aeronautics and Space Administration |
National Aeronautics and Space Administration |
National Aeronautics and Space Administration |
National Aeronautics and Space Administration |
National Aeronautics and Space Administration |
National Aeronautics and Space Administration |
National Aeronautics and Space Administration |
National Aeronautics and Space Administration |
National Aeronautics and Space Administration |
6
テクニカルペーパー
STUDIES OF CONDENSATION EFFECTS ON AIRFOIL TESTING IN THE LANGLEY 0.3-METER TRANSONIC CRYOGENIC TUNNEL
National Aeronautics and Space Administration |
National Aeronautics and Space Administration |