Results 71 to 80 of about 29,920 (238)

Analytical study of control devices for high amplitude combustion instability Quarterly report [PDF]

open access: yes
Mathematical model and analysis of combustion processes in annular rocket engines for control of high amplitude combustion ...
Burstein, S. Z., Schechter, H.
core   +1 more source

Rocket propellant injector Patent [PDF]

open access: yes, 1960
Propellant injectors for rocket combustion ...
Mantler, R. L.
core   +1 more source

Combustion instability research Summary report, 1970 [PDF]

open access: yes
Combustion instability in liquid rocket ...
Bracco, F. V.   +9 more
core   +1 more source

Investigation of the existing methods for designing pre-combustion chambers in hybrid rocket engines

open access: yesАвіаційно-космічна техніка та технологія
Hybrid propellant rocket engines (HPRE) have been under development and advancement since the beginning of rocket propulsion research, alongside liquid and solid propellant rocket motors.
Maurício Sá Gontijo
doaj   +1 more source

Technology of computational analysis of the working process parameters of low-thrust rocket engines running on gaseous oxygen-hydrogen fuel with the use of ANSYS CFD

open access: yesВестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, 2019
The paper presents the description of a mathematical model of the working process of a low-thrust rocket engine operating on gaseous oxygen-hydrogen fuel and some fragments of the technology of computational analysis of distribution of gas-dynamic ...
V. V. Ryzhkov, I. I. Morozov
doaj   +1 more source

Overview of Al-based nanoenergetic ingredients for solid rocket propulsion

open access: yesDefence Technology, 2018
The introduction of nano-sized energetic ingredients first occurred in Russia about 60 years ago and arose great expectations in the rocket propulsion community, thanks to the higher energy densities and faster energy release rates exhibited with respect
Luigi T. DeLuca
doaj   +1 more source

Summary of combustion instability research at Princeton University, 1969 [PDF]

open access: yes
Control and causes of combustion instability in rocket ...
Bracco, P. V.   +11 more
core   +1 more source

Oscillatory combustion in rockets Third semiannual report, Jun. 1 - Nov. 30, 1965 [PDF]

open access: yes
Rocket engine oscillatory combustion ...
Goluba, R.   +5 more
core   +1 more source

Control of transverse instability in rocket combustors Patent [PDF]

open access: yes, 1967
Rocket combustion chamber stability by controlling transverse instability during propellant ...
Feiler, C. E., Heidmann, M. F.
core   +1 more source

Home - About - Disclaimer - Privacy