The following pages link to (Q3148454):
Displaying 25 items.
- Complex conservative difference schemes for computing supersonic flows past simple aerodynamic forms (Q266099) (← links)
- Numerical investigation on the flowfield of ``swallowtail'' cavity for supersonic mixing enhancement (Q362008) (← links)
- Numerical investigation of supersonic flow for axisymmetric cones (Q609088) (← links)
- A numerical study of supersonic turbulence (Q1202411) (← links)
- On flux-extrapolation at supersonic outflow boundaries (Q1294612) (← links)
- Simulation of crossflow instability on a supersonic highly swept wing (Q1818733) (← links)
- Numerical simulation of supersonic flow past reentry capsules (Q1956793) (← links)
- Numerical study on the supersonic near-wake flow structures of a cylinder at an angle of attack (Q2245465) (← links)
- Simulation of a supersonic flowfield in the tip vortex core at Mach number of 6 (Q2844550) (← links)
- Mathematical simulation of supersonic airflow around the rotary body (Q2932469) (← links)
- (Q3056682) (← links)
- Numerical simulation of supersonic variable-density gas flow past a sphere (Q3481392) (← links)
- Asymmetric separated flows at supersonic speeds (Q3990001) (← links)
- Simulation of supersonic and hypersonic flows (Q4000708) (← links)
- Numerical simulation of three‐dimensional supersonic flow around aerodynamic configurations (Q4021041) (← links)
- (Q4269351) (← links)
- (Q4287269) (← links)
- Navier-Stokes simulations of slender axisymmetric shapes in supersonic, turbulent flow (Q4317329) (← links)
- (Q4511163) (← links)
- Numerical simulation of supersonic flows in a channel (Q4910026) (← links)
- LARGE-EDDY SIMULATION OF OPPOSING-JET-PERTURBED SUPERSONIC FLOWS PAST A HEMISPHERICAL NOSE (Q4929598) (← links)
- Numerical investigation of transitional supersonic axisymmetric wakes (Q5394334) (← links)
- (Q5749076) (← links)
- Flow simulation of NAL experimental supersonic airplane/booster separation using overset unstructured grids (Q5942607) (← links)
- Evaluation of the SU2 Open-Source Code for a Hypersonic Flow at Mach Number 5 (Q6161171) (← links)
