Pages that link to "Item:Q1434579"
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The following pages link to Numerical study on supersonic combustion with cavity-based fuel injection (Q1434579):
Displaying 8 items.
- Study on the influences of interaction behaviors between multiple combustion-gas jets on expansion characteristics of Taylor cavities (Q314691) (← links)
- Drag force investigation of cavities with different geometric configurations in supersonic flow (Q412883) (← links)
- Inverse estimation of inlet parameters in an axisymmetric cylindrical combustor with thermal radiation effect (Q656746) (← links)
- Heat transfer -- a review of 2004 literature (Q708974) (← links)
- Inverse estimation of inlet parameters in diffusion-controlled turbulent combustion in an axisymmetric combustor (Q992945) (← links)
- MODELING OF SUPERSONIC COMBUSTION USING POINT IMPLICIT FINITE VOLUME METHOD (Q3056056) (← links)
- Numerical analysis of supersonic combustion ramjet with upstream fuel injection (Q4447047) (← links)
- Supersonic Combustion in Air-Breathing Propulsion Systems for Hypersonic Flight (Q4634876) (← links)
