References
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- Boetcher, S. K. S. and Sparrow, E. M., 2007, "Limitations of the Standard Bernoulli Equation Method for Evaluating Pitot/Impact Tube Data," Int. J. of Heat and Mass Transfer, Vol. 50, pp. 782-788 https://doi.org/10.1016/j.ijheatmasstransfer.2006.01.044
- "FLUENT User's Guide," FLUENT Inc, 1998
- Baldwin, B. S. and Barth, T. J., "A One-Equation Turbulence Transport Model for High Reynolds Number Wall-Bounded Flows," AIAA Paper 91-0610
- Klaus, A. Hoffmann, 2000, "Computational Fluid Dynamics Volume III," 4th Edition, EESbooks
- Gracey, W., Letko, W. and Russel, W. R., 1951, "Wind-Tunnel Investigation of a Number of Total Pressure Tubes at High Angle of Attack . Subsonic Speed," NACA TN 2261
- Myers, R. H., 1995, "Response Surface Methodology," John Wiley & Sons Inc
- "Design Expert 6.0 User's Guide," Response Surface Method (RSM) Tutorials, 2003
- Gracey, W., Elwood, S., 1951, "Flight Inves tigation of the Variation of Static-Pressure Error of a Static-Pressure Tube with Distance Ahead of a Wing and a Fuselage," NACA TN 2311
- Lee, S. W. and Yoon, T. J. 1997, "Experimental Investigation of Flow Parameters Influencing the Calibration of Five-Hole Prebes," J. of KSME(B), Vol. 21, No. 5, pp. 637-649
- Lee, S. W. and Yoon, T. J. 1996, "Effect of Wall Proximity on the Calibration of a Miniature Cone-Type Five-Hole Probe," J. of KSME(B), Vol. 20, No. 8, pp. 2693-2706
- "Pitot-Static Tube, L-Shaped, Compensated General Specification for Military Specification," MIL-P-83206B, 31 1978