Pages that link to "Item:Q1672392"
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The following pages link to Optimal axisymmetric noses of bodies in a flow. Calculations and experiments (Q1672392):
Displaying 8 items.
- Analytical solution in the problem of constructing axisymmetric noses with minimum wave drag (Q604597) (← links)
- Bodies of minimal wave drag in a swirling hypersonic flow (Q797411) (← links)
- The construction of the optimal contour of the leading edge of a body in a supersonic flow (Q1370007) (← links)
- Approximation of the base pressure and determination of the optimal height of the rear face of a two-dimensional afterbody (Q1403646) (← links)
- A Karhunen-Loève least-squares technique for optimization of geometry of a blunt body in supersonic flow. (Q1428669) (← links)
- Nose part of the body of revolution having minimum aerodynamic drag in the range of large subsonic velocities (Q2086787) (← links)
- Boundary layer dynamics in a compressible gas. Numerical simulation (Q2086800) (← links)
- Erratum to: Optimal axisymmetric noses of bodies in a flow. Calculations and experiments (Q2418499) (← links)
