Results 141 to 150 of about 1,551 (188)

On Destructive Liquid Rocket Resonant Combustion

44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2008
*Experience indicates that the most destructive form of liquid rocket combustion instability is characterized by a steep-fronted, high-amplitude pressure wave sweeping through the combustion chamber in the form of a spinning tangential mode resonance.
Ron Litchford, Weiwei Luo
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Hybrid rocket combustion with prevaporized zone

Aircraft Engineering and Aerospace Technology, 2013
PurposeLow combustion completeness has been the main defect of hybrid rockets. The present study tries to address the problem by bringing up the setup of the precombustion zone, which do not increase the manufacture cost and complexity.Design/methodology/approachA precombustion zone can provide a space for the liquid oxidizer to vaporize before ...
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Bifurcation of liquid rocket combustion

34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 1998
Renat Doulatov, Victor Beliy, Igor Rossikhin   +2 more
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Resonant Combustion in Rockets

Scientific American, 1968
J. George Sotter, Gary A. Flandro
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ML for Rocket Combustion Data [PDF]

, 2022
Rüttgers, Alexander, Petrarolo, Anna
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Boron Combustion Characteristics in Ducted Rockets

Combustion Science and Technology, 1972
Abstract A test program was performed with the objective of experimentally investigating the boron reaction characteristics in a ducted rocket by systematically varying the primary chamber conditions. In order to vary the primary chamber conditions a test device was used which burned boron powder and gaseous propellants (hydrogen or carbon monoxide ...
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Experimental solid rocket combustion instability

Symposium (International) on Combustion, 1965
Experience with oscillatory combustion of solid rocket propellants is classified into three categories referred to as high-, intermediate-, and low-frequency instability. In the frequency range 1000 cps and up, instability (a) is usually encountered in transverse modes of the rocket motor; (b) results from interaction between acoustic pressure and the
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Combustion Instability in Gas Rockets

AIAA Journal, 1965
C. T. BOWMAN, I. GLASSMAN, L. CROCCO
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Transient combustion in hybrid rockets

31st Joint Propulsion Conference and Exhibit, 1995
M Karabeyoglu, D Altman, D Bershader
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Air-Turbo-Rocket combustion

33rd Aerospace Sciences Meeting and Exhibit, 1995
M Thomas, A Leonard
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