AI Mengqi, MA Yumin, ZHANG Yanjun. Analysis method of the effects of skin waviness based on RVSM operation requirement[J]. 2023, 41(11): 20-27.DOI: 10.7638/kqdlxxb-2022.0158.
Analysis method of the effects of skin waviness based on RVSM operation requirement
Skin waviness near the static pressure source affect the accuracy of altitude measurement and the airworthiness of the aircraft's RVSM operational capability. Therefore
it is necessary to evaluate the effect of small-scale skin waviness. A fast analysis method based on the small disturbance hypothesis and a numerical calculation method based on CFD were established to study the pressure effect of the waviness
and the methods were verified by the wind tunnel test data. The results show that the numerical calculation method can be used to evaluate and analyze the effects of skin waviness with high accuracy. According to the statistical analysis
the pressure deviation between the calculated value and the test value of 97.8% of the 900 pressure-measuring holes is within ± 0.002. The influence of pressure on skin waviness can be obtained accurately and quickly by the modified fast analysis method
which can be used as a rapid evaluation method for related engineering problems.
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references
Department of Aircraft Airworthiness Certification, Civil Aviation Administration of China. Aircraft airworthiness approval on the implementation of a 300m (1000 ft) vertical separation minimum in RVSM airspace: AC-21-13[S]. Beijing: Civil Aviation Administration of China, 2007(in Chinese).
YU Z J, ZHANG D X. Research on RVSM airworthiness and its related problems[J]. Advances in Aeronautical Science and Engineering, 2015, 6(1): 116-121. (in Chinese)
QU F Z, ZHANG W X. Flight test technology of reducing vertical interval for civil transport aircraft[J]. China Science and Technology Information, 2018(7): 33-35, 12. (in Chinese)
XU J C. The altimetry system error analysis and reduction due to airframe-to-airframe variability for RVSM certification[J]. Civil Aircarft Design Research, 2012(2): 28-31. (in Chinese)
VELEY M J, LEVY D W, FIORE E E. Reduced vertical separation minimum for general aviation aircraft[C]// SAE Technical Paper Series, 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 1997: 229- 240. doi: 10.4271/971494
ZHOU F, ZHAO K L, ZHANG M, et al. Static Port orientation rule for civil aircraft[J]. Acta Aerodynamica Sinica, 2017, 35(6): 823-827. (in Chinese)
ZHOU G Z. Static Port area inspection and evaluation for boeing 737NG aircraft[J]. Aeronautical Manufacturing Technology, 2014, 57(14): 77-79. (in Chinese)
ZHAO B B, DONG W J. Sensitivity analysis of waviness parameters[J]. China Science and Technology Information, 2017(15): 25-27. (in Chinese)
ZHOU X, YANG S P, ZHONG Y. Study on aerodynamic design of static pressure source based on RVSM performance requirements of civil aircraft[J]. Machine Design and Manufacturing Engineering, 2022, 51(4): 54-58. (in Chinese)
LI D P, ZHANG D Y, XIANG C T. CFD calculation method of the influence of civil aircraft skin waviness on altimetry system[J]. China Science and Technology Information, 2019(20): 30-31. (in Chinese)
JIN D, WU J. A new analysis method of aircraft surface waviness based on 3D measurement technology[J]. Advances in Aeronautical Science and Engineering, 2013, 4(1): 85-89. (in Chinese)
ZHANG L, WU Z L. A calculation method of aircraft surface waviness based on the method of point projection on curved surface[J]. Journal of Graphics, 2016, 37(5): 626-631. (in Chinese)
MA M, CAO X F, LI Q M, et al. An approach to analyzing skin surface waviness of civil aircraft based on wavelet filtering[J]. Science Technology and Engineering, 2013, 13(35): 10750-10754. (in Chinese)
WU Z N. Aerodynamics[M]. Beijing: Beijing University of Aeronautics Astronautics Press, 2016 (in Chinese).