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arXiv:2406. 03884v1 [math. AP] 6 Jun 2024 lays an important role in aerodynamics Mathematically, the study of the contact discontinuity for steady compressible flows can be classified into three categories: subsonic-subsonic flow, supersonic-supersonic flow and subsonic supersonic flow (i e , transonic flow) Much mathematical progress
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Improvement of weighted compact scheme with multi-step . . . In this paper, a multi-step strategy is pro- posed to increase the accuracy of the CRWENO scheme near discontinuities Instead of constructing the fth order compact scheme directly from three third
Status and Advances in Commercial Supersonic Technology Training the next generation of researchers to understand the design drivers for low-speed aerodynamics and handling characteristics of low-boom supersonic configurations
PREDICTIONS FOR PROJECTILES AT TRANSONIC AND SUPERSONIC SPEEDS Thus, a NavieriStokes computational procedure is used in this report to predict the individual drag components and test the accuracy of the predictions of the design codes A thin'-layer Navier4Stokes code has been used to compute the entire flow field over projectiles including the base region Numerical calcu-lations have been made for various Mach numbers in the transonic and supersonic