, 2009 A fictional work combining text and illustrations published as part of Artis Den Bosch's 'Post Producktie' series of artist's books.
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Design and performance study of side water inlet device of underwater vehicle engine
Xibei Gongye Daxue XuebaoMetal water fuel engines possess advantages such as high energy and specific impulse, simple structure, and safe and pollution-free fuel, making them suitable for underwater supercavitating vehicles.
LIU Lin +4 more
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Effect of Nanoparticle Concentration on Physical and Heat-Transfer Properties and Evaporation Characteristics of Graphite/n-Decane Nanofluid Fuels. [PDF]
ACS Omega, 2022 Li S +6 more
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Advanced ramjet concepts program [PDF]
Uniquely advantageous features, on both the performance and weight sides of the ledger, can be achieved through synergistic design integration of airbreathing and rocket technologies in the development of advanced orbital space transport propulsion ...
Leingang, J. L.
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Hypersonic ramjet experiment project. Phase 1: Computer program description, ramjet and scramjet cycle performance [PDF]
A computer program was developed to describe the performance of ramjet and scramjet cycles. The program performs one dimensional calculations of the equilibrium, real-gas internal flow properties of the engine. The program can be used for the following: (
Jackson, R. J., Wang, T. T.
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Microstructure and Mechanical Properties of Unidirectional, Laminated Cf/SiC Composites with α-Al2O3 Nanoparticles as Filler. [PDF]
Nanomaterials (Basel), 2022 Yang L, Wang F, Liao J, Chen Z, Kou Z.
europepmc +1 more source
System controls challenges of hypersonic combined-cycle engine powered vehicles [PDF]
Hypersonic aircraft with air-breathing engines have been described as the most complex and challenging air/space vehicle designs ever attempted. This is particularly true for aircraft designed to accelerate to orbital velocities.
Ianculescu, George D. +1 more
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Time-Varying Oscillatory Response of Burning Gel Fuel Droplets. [PDF]
Gels, 2023 Sharma J, Miglani A.
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Rocket Based Combined Cycle (RBCC) Propulsion Technology Workshop. Volume 1: Executive summary [PDF]
The goal of the Rocket-Based Combined Cycle (RBCC) Propulsion Technology Workshop was to assess the RBCC propulsion system's viability for Earth-to-Orbit (ETO) transportation systems.
Chojnacki, Kent T.
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Calculation method of gas flow of a ramjet engine [PDF]
, 2017 In the present study calculations algorithm of gas flow of ramjet engine are shown. The algorithm is based on the solution of two-dimensional gas dynamics equations. Calculations are done for ramjet model which consists of air intake, combustion chamber,
Кагенов, А. М. +2 more
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