Рассматривается течение водородо-воздушной горючей смеси в канале переменного
сечения, представляющего собой два последовательно расположенных сопла Лаваля …

The ignition behavior of hypergolic propellants is of importance for rocket applications that
require multiple restarts and/or thrust control. Additionally the high specific impulse and low …

Traditional hypergolic propellant combinations, such as those used on the space shuttle
orbital maneuvering system first flown in 1981, feature hydrazine based fuels and nitrogen …

Understanding hypergolic ignition is critical for the safe and successful operation of
hypergolic engines. The complex coupling of physical and chemical processes during …

Present study reports on the hypergolic combustion characteristics. Numerical simulation of
hypergolic combustion is performed where hypergolicity of the MMH–RFNA combination in …

The combustion of gas-gas hypergolic propellants with MMH (Monomethylhydrazine) as fuel
and RFNA (Red fuming nitric acid) as oxidizer are studied numerically for unlike impinging …

Hypergolic systems rely on fuel and oxidizer propellant combinations that spontaneously
ignite upon contact. Monomethylhydrazine (MMH) fuel and nitrogen tetroxide (NTO)-based …

The authors studied the case of (H 2+ 0.5 O 2+ 1.881 N 2) hydrogen-air mixture combustion
in the stationary detonation wave. Analysis of possible flow patterns with stationary …

PURDUE UNIVERSITY Page 1 Graduate School ETD Form 9 (Revised 01/14) PURDUE
UNIVERSITY GRADUATE SCHOOL Thesis/Dissertation Acceptance This is to certify that the …