6Latif 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.
7Masud J, Qazi O A, Sheikh S R, et al. Adjustment of aerodynamic compensation characteristics of a pitot tube by rear-body shape manipulation[R]. AIAA-2008-254, 2008.
8Masud J, Afgan I. Performance characteristics of flush angle-of-attack measurement system integrated on a pitot tube[R]. AIAA-2009-1077, 2009.
9ShihT H, Liou WW, Shabbir A, et al. A new,κ-ε eddy viscosity model for high Reynolds number turbulent flows [J]. ComputFluids, 1995, 24(3): 227-238.
10MIL-P-26292c(a)NOT2, Pitot and static pressure sys- tems, installation and inspection of (no s/s document) [S]. 1998.