Results 131 to 140 of about 342 (196)

Abrasive Waterjet Machining. [PDF]

Materials (Basel)
Hashish M.
europepmc   +1 more source

A review on aero-engine inlet-compressor integration and inlet flow distortion in axial compressors. [PDF]

Fundam Res
Li Z, Sun D, Dong X, Sun X.
europepmc   +1 more source

Advances in Synthesis and Ignition Performance of Ionic Liquid-Hydrogen Peroxide Green Propellants. [PDF]

Molecules
Zhang Y, Zhang X, Yin D, Zhang Q.
europepmc   +1 more source

Smart Manufacturing for High-Performance Materials: Advances, Challenges, and Future Directions. [PDF]

Materials (Basel)
Antony Jose S, Tonner A, Feliciano M, Roy T, Shackleford A, Menezes PL.   +5 more
europepmc   +1 more source

Experimental investigation and parametric optimization of machinability and surface characteristics in wire EDM of Inconel 718. [PDF]

Sci Rep
Kar S, C A N, N R P, Majumder T, Baroi BK, Kebede AW.   +5 more
europepmc   +1 more source

Comparative Study on Extrusion 3D Printing of Solid Propellant Based on Plunger and Screw. [PDF]

Materials (Basel)
Song S, Shi J, Ren Q, Miao K, Tang M, Shi H.   +5 more
europepmc   +1 more source

Mitigating hypersonic heat barrier via direct cooling enhanced by leidenfrost inhibition. [PDF]

Nat Commun
Wang JX, Zhong M, Li JX, Wang S, Bian J, Mao Y, Wang H.   +6 more
europepmc   +1 more source

Additive Manufacturing of Aerospace Composites: A Critical Review of the Material-Process-Design Interplay and Prospects for Application. [PDF]

Materials (Basel)
Shen C, Guo Y, Shen Z, Yan F, Zhong N.
europepmc   +1 more source

Recent Trends in Non-Destructive Testing Approaches for Composite Materials: A Review of Successful Implementations. [PDF]

Materials (Basel)
Tai JL, Sultan MTH, Łukaszewicz A, Józwik J, Oksiuta Z, Shahar FS.   +5 more
europepmc   +1 more source

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Numerical investigations of hybrid rocket engines

Acta Astronautica, 2018
Abstract Paper presents the results of numerical studies of hybrid rocket engines operating cycle including unsteady-state transition stage. A mathematical model is developed accounting for the peculiarities of diffusion combustion of fuel in the flow of oxidant, which is composed of oxygen-nitrogen mixture.
V.B. Betelin, A.G. Kushnirenko, N.N. Smirnov, V.F. Nikitin, V.V. Tyurenkova, L.I. Stamov   +5 more
openaire   +3 more sources