The prediction of nozzle performance and heat transfer in hydrogen/oxygen rocket engines with transpiration cooling, film cooling, and high area ratios

High temperature furnace modeling and performance verifications

James E. Smith undifferentiated

Heat transfer, 1986

International Heat Transfer Conference (8th 1986 San Francisco, Calif.)

High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation

Robert S. Jankovsky

Navier-Stokes analysis of turbine blade heat transfer

Robert J. Boyle

Computational heat transfer

A. A. Samarskiĭ

Finite-element reentry heat-transfer analysis of space shuttle orbiter

William L. Ko

Stagnation-point heat-transfer rate predictions at aeroassist flight conditions

Roop N. Gupta

Heat transfer on a film-cooled blade

Vijay K. Garg