Zobrazeno 1 - 10
of 10
pro vyhledávání: '"ZHONG Shidong"'
Publikováno v:
Hangkong gongcheng jinzhan, Vol 14, Iss 2, Pp 35-43 (2023)
Sonic boom suppression is a key technology that must be broken through in the development of a new generation of supersonic civil aircraft. The reasonable design of configuration parameters can make the aircraft have good sonic boom characteristics.
Externí odkaz:
https://doaj.org/article/b87e91cc093747659c2442ca50aff3c2
Publikováno v:
Hangkong gongcheng jinzhan, Vol 13, Iss 2, Pp 9-17 (2022)
The study on the lift enhancement effect of the retractable belly flap on the flying wing configuration can conclude the effect rules on aircraft aerodynamic force. A flying wing configuration model is taken as the initial shape of flying wing config
Externí odkaz:
https://doaj.org/article/6ad41beb135d484d94fa9c7284d2b3a4
Publikováno v:
Hangkong gongcheng jinzhan, Vol 13, Iss 6, Pp 107-115,133 (2022)
Reduction of trim loss is essential to raise lift-to-drag ratio and enhance flight control performance for flying wing configuration,so the influence on aerodynamic optimization of transonic flying wing configuration is studied based on discrete adjo
Externí odkaz:
https://doaj.org/article/4fd1effdd9ac4c78b3688eddaa57d188
Akademický článek
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Publikováno v:
International Journal of Modern Physics B. 34:2040101
Usually, force tests and pressure tests are conducted with different model in wind tunnel which could cause trouble for aircraft design as the pressure test results always could not match the force test results. So attempts to do force tests along wi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a15e7ec7fd258e3f97dd5b8673cef264
https://doi.org/10.1142/s0217979220401013
https://doi.org/10.1142/s0217979220401013
Publikováno v:
In Theoretical and Applied Mechanics Letters November 2017 7(6):325-330
Publikováno v:
21st AIAA International Space Planes and Hypersonics Technologies Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2faf0be4f9da95b586b7f02abd3ed30f
https://doi.org/10.2514/6.2017-2171
https://doi.org/10.2514/6.2017-2171
Publikováno v:
2014 Fifth International Conference on Intelligent Systems Design and Engineering Applications.
For supercritical flow over the surface airfoil, the supersonic zone may be terminated by a strong normal shock. The porous surface with cavity is a passive shock wave/boundary layer control to reduce the wave drag. The effect of porous surface on th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::311c24487f193a758af5e65c03321c2b
https://doi.org/10.1109/isdea.2014.76
https://doi.org/10.1109/isdea.2014.76
Publikováno v:
Acta Aerodynamica Sinica / Kongqi Donglixue Xuebao. feb2016, Vol. 34 Issue 1, p113-118. 6p.
Publikováno v:
Acta Aerodynamica Sinica / Kongqi Donglixue Xuebao. feb2016, Vol. 34 Issue 1, p107-130. 7p.