A fully implicit time accurate method for hypersonic combustion View on Open Library

A fully implicit time accurate method for hypersonic combustion

by Shaye Yungster

No reviews yet
First published: 1994 1 language

Reviews

Log in or sign up to write a review.

No reviews yet. Be the first!

More by Shaye Yungster

Navier-Stokes simulation of the supersonic combustion flowfield in a ram accelerator

Navier-Stokes simulation of the superson...

Multiple-cycle simulation of a pulse detonation engine ejector

Multiple-cycle simulation of a pulse det...

Numerical study of shock-induced combustion in methane-air mixtures

Numerical study of shock-induced combust...

Computational study of near-limit propagation of detonation in hydrogen-air mixtures

Computational study of near-limit propag...

Computational study of flow establishment in a ram accelerator

Computational study of flow establishmen...

Numerical simulation of shock-induced combustion generated by high-speed projectiles in detonable gas mixtures

Numerical simulation of shock-induced co...