Works matching DE "SHOCK tunnels"
Results: 10
Flow of a dispersed phase in the Laval nozzle and in the test section of a two-phase hypersonic shock tunnel.
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- Journal of Applied Mechanics & Technical Physics, 2008, v. 49, n. 5, p. 789, doi. 10.1007/s10808-008-0099-y
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- Article
Evaluation of Kinetic Models for Autoignition of Automotive Reference Fuels in HCCI Applications.
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- Turkish Journal of Engineering & Environmental Sciences, 2007, v. 31, n. 6, p. 383
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- Article
Combustion Phenomena within a RBCC Engine under Scramjet-mode Operation.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 71
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- Article
Modern developments in hypersonic wind tunnels.
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- Aeronautical Journal, 2006, v. 110, n. 1103, p. 21, doi. 10.1017/S0001924000004346
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- Article
Investigation of Slender Bodies at Hypersonic Mach Numbers.
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- Fluid Dynamics, 2021, v. 56, n. 2, p. 255, doi. 10.1134/S0015462821020087
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- Article
Development, Uniformity and Peak Heating of a Hypersonic Laminar Near-Wake Flow.
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- International Journal of Aerospace Innovations, 2012, v. 4, n. 3/4, p. 119, doi. 10.1260/1757-2258.4.3-4.119
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- Article
High speed schlieren facility for visualization of flow fields in hypersonic shock tunnels.
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- Current Science (00113891), 2007, v. 92, n. 1, p. 56
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- Article
Proximal bodies in hypersonic flow.
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- Journal of Fluid Mechanics, 2007, v. 590, n. 1, p. 209
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- Article
Visualization of Shock Wave Phenomenon around a Sharp Cone Model at Hypersonic Mach Number in a Shock Tunnel using High Speed Schlieren Facility.
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- Journal of Applied Fluid Mechanics, 2019, v. 12, n. 2, p. 461, doi. 10.29252/jafm.12.02.29250
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- Article
Experimental investigation of drag reduction by forward facing high speed gas jet for a large angle blunt cone at Mach 8.
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- Sādhanā: Academy Proceedings in Engineering Sciences, 2007, v. 32, n. 1/2, p. 123, doi. 10.1007/s12046-007-0011-0
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- Article