Results 221 to 230 of about 82,587 (286)
Poster: Bow Shock Instability at Hypersonic Speed
Alberto Álvarez, Adrian Lozano-Durán
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A Highly Spatiotemporal Resolved Pyrometry for Combustion Temperature Measurement of Single Microparticles Applied in Powder-Fueled Ramjets. [PDF]
Wang Z+7 more
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Influence of plasma-enhanced combustion on RBCC engine using URANS. [PDF]
Zhang WR, Liu YS, Zou XR, Xu C, Xue R.
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Effect of Yb on Microstructure and Mechanical Properties of Al-Cu-Mn Heat-Resistant Aluminum Alloys. [PDF]
Huang C+5 more
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Acoustic Actuators for the Manipulation of Micro/Nanorobots: State-of-the-Art and Future Outlooks. [PDF]
Cao HX+4 more
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Mesoscopic Kinetic Approach of Nonequilibrium Effects for Shock Waves. [PDF]
Qiu R, Yang X, Bao Y, You Y, Jin H.
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Gas migration characteristics in vehicle tank under different ventilation conditions. [PDF]
Wang Y, Yang C, Liu Y, Li X.
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Adding Value at Hypersonic Speed
45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2009In the test and evaluation (T&E) world, obtaining critical ground-test data requires that the effort be approached as a value-added task. By acquiring the ground-test data faster and cheaper, value is added to the overall flight system development program. At the Arnold Engineering Development Center (AEDC), a culture of maximizing the value of all T&E
Dusty Vaughn+2 more
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Sublimation of graphite at hypersonic speeds
AIAA Journal, 1965In this paper, a new theoretical model is presented for the sublimation of graphite at hypersonic flight speeds. The aerothermochemical interactions between dissociated air and graphite are treated by means of a nine-component model, including O, O2, N, N2, CO, CO2, C, C3, and CN.
Leon M. GlLBERT, SlNCLAIRE M. Scala
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