Pages that link to "Item:Q604616"
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The following pages link to Numerical modeling of the effect of geometric asymmetry on the damping aerodynamic characteristics of supersonic sectional flight vehicles (Q604616):
Displaying 4 items.
- Method of determining the aerodynamic coefficients of asymmetric bodies with allowance for nonlinear body shape influence factors (Q1317698) (← links)
- Aerodynamic equivalence of asymmetric bodies with allowance for nonlinear body shape influence factors and angle of attack (Q1339625) (← links)
- Study of the damping characteristics of sectional flight vehicles of different length (Q2269416) (← links)
- Determining the time-dependent aerodynamic characteristics by calculating the steady-state flow past vehicles with a modified cross-sectional shape (Q2388102) (← links)