Pages that link to "Item:Q2747797"
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The following pages link to Numerical computations of supersonic inlet flow (Q2747797):
Displaying 14 items.
- Complex conservative difference schemes for computing supersonic flows past simple aerodynamic forms (Q266099) (← links)
- A computational study of the effect of angles of attack on a double-cone type supersonic inlet with a bleeding system (Q365519) (← links)
- Computational study of flow in a rocket-based combined cycle (RBCC) engine inlet (Q1043164) (← links)
- Computation of steady supersonic flows by a flux-difference/splitting method (Q1069378) (← links)
- Calculation of the performance characteristics of a three-dimensional scramjet nozzle/afterbody system (Q1569354) (← links)
- Numerical simulation of supersonic flow past reentry capsules (Q1956793) (← links)
- Mixed compression air-intake design for high-speed transportation (Q2089453) (← links)
- Viscous flow in a mixed compression intake (Q2892502) (← links)
- Finite Element Computation of Buzz Instability in Supersonic Air Intakes (Q2962438) (← links)
- Details on the Computation of Hypersonic Inlet Flows (Q3061467) (← links)
- Three-dimensional flow simulations for supersonic mixed-compression inlets at incidence (Q3216332) (← links)
- Calculation of supersonic flows with heat addition (Q3348615) (← links)
- Numerical simulation of supersonic flows in a channel (Q4910026) (← links)
- (Q5749076) (← links)