Rocket engines -- Combustion

High altitude chemically reacting gas particle mixtures.

prepared for National Aeronautics and Space Administration, Aerodynamic Systems Analysis Section ; by S.D. Smith.

Identification and management of filament-wound case stiffness parameters

V. Verderaime and M. Rheinfurth.

SSME thrust chamber simulation using Navier Stokes equations: final report

by A.J. Przekwas, A.K. Singhal and L.T. Tam ; prepared for National Aeronautics and Space Administration, Marshall Space Flight Center

ALS rocket engine combustion devices: design and demonstration

prepared by Steve Arreguin.

Modeling on nonacoustic combustion instability in simulations of hybrid motor tests

M. Rocker.

Liquid rocket engine nozzles

written by J. C. Hyde and G. S. Gill; edited by Russell B. Keller, Jr.

Analysis of the measured effects of the principal exhaust effluents from solid rocket motors

R. Dawbarn, M. Kinslow, and D. J. Watson

Engine data interpretation system (EDIS) (Phase II)

prepared by Thomas L. Cost and Martin O. Hofmann.

A premixed hydrogen/oxygen catalytic igniter

James M. Green.

Combustion instability in liquid and solid propellant rockets

Library of Congress. Aerospace Technology Division.