Pages that link to "Item:Q939949"
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The following pages link to Computation of field structure and aerodynamic characteristics of delta wings at high angles of attack (Q939949):
Displaying 6 items.
- Aerodynamic characteristics of a deltawing in the case of harmonic oscillations with respect to the roll and yaw angles at high angles of attack (Q359316) (← links)
- Sharp maximal inequalities for stochastic processes (Q492175) (← links)
- Numerical investigation of vortical flows over a close-coupled delta canard-wing configuration (Q2245209) (← links)
- Thermal effect of the slanted surface around the central hole of a miniature delta wing on the leading-edge vortices (Q2873394) (← links)
- Numerical simulation of flow over delta wing with trailing-edge jet at high angle of attack (Q3157074) (← links)
- Numerical Computation of Vortical Flow Fields of Double‐Delta Wings Moving in a Compressible Viscous Medium (Q4319389) (← links)