| [1] Garcy W. Measurement of aircraft speed and altitude. NASA Reference Publication 1046, 1980.[2] Letko W. Investigation of the fuselage interference on a pitot-static tube extending forward from the nose of the fuselage. NACA-TN-1496, 1947.[3] White F M. Viscous fluid flow[M]. New York: McGraw-Hill, 1991: 500-562.[4] Schreier S. Compressible flow[M]. New York: Wiley, 1982: 133-200.[5] Ames Research Staff. Equations, tables, and charts for compressible flow. NACA Report 1135, 1953.[6] Ritchie V S. Several methods for aerodynamic reduction of static-pressure sensing errors for aircraft at subsonic, near-sonic, and low supersonic speeds. NASA TR R-18, 1959.[7] Lao S, Bao Y. Computation of transonic aerodynamically compensating pitot tube[J]. Journal of Aircraft, 1988, 25(6): 544-547.[8] Swafford T W, Bomba J, Daiber M P. Computational evaluation of compensated pitot-static probes using the Euler equations. AIAA-1995-1839, 1995.[9] 武文康, 屠兴. 气动补偿空速管的研究与发展[J]. 气动试验与测量控制, 1993, 7(4): 11-16. Wu Wenkang, Tu Xing. The research and development of the aerodynamic compensated pitot-static tube[J]. Aerodynamic Experiment and Measurement & Control, 1993, 7(4): 11-16. (in Chinese)[10] 汤黄华. 机头空速管位置误差值的计算[J]. 洪都科技, 1991(4): 1-11. Tang Huanghua. Calculation of nose pitot tube position error[J]. Hongdu Science and Technology, 1991(4): 1-11. (in Chinese)[11] 汤黄华. 补偿空速管与飞机的匹配性设计[J]. 洪都科技, 1998(4): 16-23. Tang Huanghua. Compatibility design of pitot tube compensating with aircraft[J]. Hongdu Science and Technology, 1998(4): 16-23. (in Chinese)[12] Latif A, Masud J, Sheikh S R, et al. Robust design of an aerodynamic compensation pitot-static tube for supersonic aircraft[J]. Journal of Aircraft, 2007, 44(1): 163-169.[13] Masud J, Qazi O A, Sheikh S R, et al. Adjustment of aerodynamic compensation characteristics of a pitot tube by rear-body shape manipulation. AIAA-2008-254, 2008.[14] Masud J, Afgan I. Performance characteristics of flush angle-of-attack measurement system integrated on a pitot tube. AIAA-2009-1077, 2009.[15] Shih T H, Liou W W, Shabbir A, et al. A new k-ε eddy viscosity model for high Reynolds number turbulent flows[J]. Comput Fluids, 1995, 24(3): 227-238.[16] MIL-P-26292C(3)NOT 2, Pitot and static pressure systems, installation and inspection of (no s/s document)[S]. 1998. |
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