Results 91 to 100 of about 29,759 (245)
The effect of mixing, radiation, and finite rate combustion upon the flow field and surroundings of the exhaust plumes of rocket engines burning RP1 /kerosene/ and liquid oxygen [PDF]
Shear layer mixing, hydrocarbon oxidation, and carbon cloud radiation models for liquid rocket engine exhaust plume ...
Edelman, R., Fortune, O.
core +1 more source
How to Fish With Respect: A Transformation of Human‐Fish Relations in Riverside Amazonia
American Anthropologist, Volume 128, Issue 1, Page 63-72, March 2026.ABSTRACT Riverside inhabitants of the Middle Xingu River Basin, in the Brazilian Amazonia, frequently say that it is important to respect animals and the forest spirits who protect them. In recent decades, however, the development of an iced fish industry in the region has changed what respect means and how it is expressed when it comes to fishing ...
Vinicius de Aguiar Furuie
wiley +1 more source
The prediction of the nonlinear behavior of unstable liquid rockets [PDF]
Analytical technique for solving nonlinear combustion problems associated with liquid propellant rocket ...
Powell, E. A., Zinn, B. T.
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Summary of literature survey of hypergolic ignition spike phenomena, phase I Final report, Apr. 8 - Dec. 31, 1965 [PDF]
Summary of industry survey and literature search of ignition spike phenomena in low thrust, hypergolic, liquid bipropellant rocket ...
Christos, T., Perlee, H. E.
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Liquid Hydrogen/Liquid Oxygen Rocket Engine Technology
Journal of the Korean Society of Propulsion Engineers, 2022 Nam-Kyung Cho +3 more
openaire +1 more source
Cryogenic gel flow viscometer [PDF]
, 1972 Coiled section of tubing measures viscous properties of gelled cryogenic propellants under conditions closely resembling flow in rocket engine systems. Characteristic flow curve provides data necessary for the design of prototype hardware systems using ...
Globus, R. H., Vanderwall, E. M.
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Mehran University Research Journal of Engineering and Technology, 2019 Optimum characteristic length of the combustion chamber of liquid rocket engine is very important to get higher energy from the liquid propellants. Characteristic length is defined by the time required for complete burning of fuel.
Tajwali Khan, Ihtzaz Qamar
doaj
The physiology of survival: Space
Experimental Physiology, EarlyView.
Damian M. Bailey, Angelique van Ombergen
wiley +1 more source
Design criteria monograph for high-load high-speed rolling-contact bearings [PDF]
, 1972 Monograph was published which summarizes and systematically orders large body of successful techniques and practices developed for design of liquid rocket engine turbopump bearings.
core +1 more source
Designing and Testing of HDPE–N2O Hybrid Rocket Engine
Engineering ProceedingsHybrid Rocket Engines (HREs) combine the advantages of solid and liquid propellants, offering thrust control, simplicity, safety, and cost efficiency.
Triyan Pal Arora +6 more
doaj +1 more source