DISTINCTIVE FEATURES OF THE INTRACHAMBER INSTABILITY 
OF COMBUSTION IN LIQUID-PROPELLANT ROCKET ENGINES

V. V. Gotsulenko

UDC 629.7:533.6.001

Self-oscillations and certain of their regularities determined 
by solution of a degenerate system of differential equations that 
is used in considering combustion instability in combustion chambers 
of liquid-propellant rocket engines are modeled mathematically.

Zheltye-Vody Enterprise Institute "Strategiya," 38 Gagarin 
Str., Zheltye Vody, 52201, Ukraine. Translated from Inzhenerno-Fizicheskii 
Zhurnal, Vol. 81, No. 5, pp. 897-902, September-October, 2008. 
Original article submitted March 19, 2007; revision submitted February 
13, 2008.