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- W2387050779 abstract "The aerodynamics research of canard rolling airframe missile was summarized in this paper.The aerodynamics of rolling,canard and canard rolling were introduced.There were many kinds of votex structures in flowfield of the RAM which aerodynamics was typically non-linear and unsteady.According to numerical simulation and wind tunnel tests,it was proved that the lengthways aerodynamics were invariable,while unsteady theory was able to solve the lengthways aerodynamic problems.The nonlinear was presented by changing of angle of attack.According to stationary and non-stationary numerical simulations,it was also true that the non-stationary free vortex was the key impact factor of aerodynamic performance." @default.
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- W2387050779 date "2013-01-01" @default.
- W2387050779 modified "2023-09-22" @default.
- W2387050779 title "Research on Aerodynamics of Canard Rolling Airframe Missile" @default.
- W2387050779 hasPublicationYear "2013" @default.
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