Turbulent boundary layer wall pressure flight data

Description

Wall pressure data acquired during flight tests at three flight conditions are provided: 48k feet altitude at Mach 0.86; 32k feet at Mach 0.70; and 24k feet at Mach 0.56. Details of the flight test, sensors, and sensor locations are given in a journal article that is referenced in the supporting documents datafile.

Resources

Name Format Description Link
B101 ZIP B101.zip Open resource
B106_pt_10 ZIP B106_pt_10.zip Open resource
B106_pt_1 ZIP B106_pt_1.zip Open resource
B106_pt_2 ZIP B106_pt_2.zip Open resource
B106_pt_3 ZIP B106_pt_3.zip Open resource
B106_pt_4 ZIP B106_pt_4.zip Open resource
B106_pt_5 ZIP B106_pt_5.zip Open resource
B106_pt_6 ZIP B106_pt_6.zip Open resource
B106_pt_7 ZIP B106_pt_7.zip Open resource
B106_pt_8 ZIP B106_pt_8.zip Open resource
B106_pt_9 ZIP B106_pt_9.zip Open resource
B109_pt_10 ZIP B109_pt_10.zip Open resource
B109_pt_1 ZIP B109_pt_1.zip Open resource
B109_pt_2 ZIP B109_pt_2.zip Open resource
B109_pt_3 ZIP B109_pt_3.zip Open resource
B109_pt_4 ZIP B109_pt_4.zip Open resource
B109_pt_5 ZIP B109_pt_5.zip Open resource
B109_pt_6 ZIP B109_pt_6.zip Open resource
B109_pt_7 ZIP B109_pt_7.zip Open resource
B109_pt_8 ZIP B109_pt_8.zip Open resource
B109_pt_9 ZIP B109_pt_9.zip Open resource
Supporting Documents ZIP Docs.zip Open resource

Tags

Topics

Categories