cal_run - Sheet1 Wright Brothers Wind Tunnel Test Pressures...

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Sheet1 Page 1 Wright Brothers Wind Tunnel Test: Pressures in psf, Velocity in mph, Temperature in degrees F, and forces in volts. DateTimeVelocityVcorrMachRe/ftRecorrPitch AngleYaw Angle%RHTemperaturePstaticPtotal-PstaticLiftDragSidePitchYawRoll 3/3/20041:21:50 PM1.2351.2370.00211828.54211808.169-2045.9958.0392165.890.0040.982-0.0670.06-0.233-0.298-0.126 3/3/20041:21:51 PM1.3571.360.00213150.3513127.974-2045.9958.0162190.4440.0050.983-0.0670.059-0.232-0.298-0.126 3/3/20041:21:52 PM1.9191.9220.00318594.35418562.723-2045.9958.0132190.7320.010.982-0.0680.06-0.233-0.298-0.128 3/3/20041:21:53 PM1.8661.8690.00218078.47718047.74-2045.9957.9952190.5380.0090.981-0.0680.059-0.233-0.297-0.128 3/3/20041:21:54 PM1.2411.2430.00212024.83312004.306-2046.0558.0872192.0260.0040.981-0.0670.059-0.233-0.298-0.128 3/3/20041:21:55 PM1.8121.8150.00217555.38117525.518-2046.0557.9742190.4130.0090.981-0.0670.059-0.233-0.298-0.128 3/3/20041:21:56 PM1.0111.0130.0019799.0939782.392-2046.0558.0282190.5750.0030.982-0.0670.059-0.233-0.297-0.126 3/3/20041:21:57 PM1.191.1920.00211532.13511512.478-2046.0558.032190.4860.0040.982-0.0670.059-0.232-0.297-0.126 3/3/20041:21:58 PM1.8371.840.00217800.45917770.129-2046.0558.0212190.5440.0090.982-0.0670.059-0.233-0.297-0.124 3/3/20041:21:59 PM1.8341.8370.00217768.5817738.352-2046.0557.9792190.4410.0090.982-0.0670.059-0.232-0.296-0.123 3/3/20041:22:00 PM1.271.2730.00212309.54212288.556-2046.0558.0382190.7990.0040.982-0.0670.059-0.233-0.297-0.123
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This note was uploaded on 01/28/2012 for the course AERO 16.01 taught by Professor Markdrela during the Fall '05 term at MIT.

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