Academic literature on the topic 'Arc-jet testing'

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Journal articles on the topic "Arc-jet testing"

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White, Susan M., and Douglas Burleigh. "Infrared thermographic techniques for arc-jet testing." Journal of Spacecraft and Rockets 30, no. 4 (1993): 477–83. http://dx.doi.org/10.2514/3.25553.

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Savino, Raffaele, Mario De Stefano Fumo, Diego Paterna, and Di Maso Andrea. "Arc-Jet Testing of Ultra-High-Temperature-Ceramics." Open Aerospace Engineering Journal 3, no. 1 (2010): 20–31. http://dx.doi.org/10.2174/1874146001003010020.

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The article deals with arc-jet experiments on different Ultra High Temperature Ceramics models in high enthalpy hypersonic non equilibrium flow. Typical geometries for nose tip or wing leading edges of interest for hypersonic vehicles, as rounded wedge, hemisphere and cone are considered. Temperature measurements have been performed using pyrometers, an IR thermocamera and thermocouples. Spectral emissivity has been evaluated by suitable experimental techniques. The details of the experimental set-up, the tests procedure and the measurements are discussed in the text. The UHTC materials have b
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Savino, Raffaele, Mario De Stefano Fumo, Diego Paterna, Andrea Di Maso, and Frederic Monteverde. "Arc-jet testing of ultra-high-temperature-ceramics." Aerospace Science and Technology 14, no. 3 (2010): 178–87. http://dx.doi.org/10.1016/j.ast.2009.12.004.

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Choe, Mun Seok, Kwon Se Kim, and Doo Seuk Choi. "Study on Flame Propagation Characteristics According to New Ignition- Source in a Constant Volume Combustion Chamber." Defect and Diffusion Forum 391 (February 2019): 142–51. http://dx.doi.org/10.4028/www.scientific.net/ddf.391.142.

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This study has the purpose to consider a new ignition source in order to increase the inflammable limit of a gasoline engine at its lean region. To analyze flame propagation characteristics, a CVCC (constant volume combustion chamber) was produced, and three types of devices – conventional type, arc type, and jet type – were manufactured to conduct combustion testing. Experimental variables were the air/fuel ratio from 1.0 to 1.8 and charging pressure from 2 bar to 4 bar. The result of flame propagation analysis showed that the spread for jet type was faster than that of conventional type by 1
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Yang, Sungmo, Ilsung Choi, and Gisu Park. "Development of combined hypersonic test facility for aerothermodynamic testing." PLOS ONE 19, no. 2 (2024): e0298113. http://dx.doi.org/10.1371/journal.pone.0298113.

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In this study, a combined test facility was developed using a combination of an arc-jet tunnel and a shock tunnel for aerothermodynamic testing. The performance validation of individual parts was performed, and results were obtained from the combined test. A small-scale Huels-type arc-jet tunnel was used to preheat the test model by aerodynamic heating before conducting the experiments in the shock tunnel to duplicate the hot surfaces of flight objects encountered during hypersonic flight. The high-enthalpy flow in the arc-jet tunnel provided a heat flux of 1.99±0.03 MW/m2 for a flat-faced mod
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Mazaheri, Alireza, Walter E. Bruce, Nathaniel J. Mesick, and Kenneth Sutton. "Methodology for Flight-Relevant Arc-Jet Testing of Flexible Thermal Protection Systems." Journal of Spacecraft and Rockets 51, no. 3 (2014): 789–800. http://dx.doi.org/10.2514/1.a32721.

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Cinquegrana, Davide, Raffaele Votta, Carlo Purpura, and Eduardo Trifoni. "Continuum breakdown and surface catalysis effects in NASA arc jet testing at SCIROCCO." Aerospace Science and Technology 88 (May 2019): 258–72. http://dx.doi.org/10.1016/j.ast.2019.03.026.

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Savino, Raffaele, Mario De Stefano Fumo, Laura Silvestroni, and Diletta Sciti. "Arc-jet testing on HfB2 and HfC-based ultra-high temperature ceramic materials." Journal of the European Ceramic Society 28, no. 9 (2008): 1899–907. http://dx.doi.org/10.1016/j.jeurceramsoc.2007.11.021.

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Dickstein, Dylan, Arian Ghazari, Warren Nadvornick, et al. "Mass loss, sublimation, and surface damage of lanthanum hexaboride in an arc jet plasma." Journal of Applied Physics 133, no. 5 (2023): 055101. http://dx.doi.org/10.1063/5.0130131.

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An experimental and simulation-based approach is used to determine the effects of an arc jet plasma on the refractory ceramic material lanthanum hexaboride ([Formula: see text]). Experiments are performed at the High Energy Flux Test facilitY (HEFTY) located at UCLA. An SG-100 plasma jet generates an argon plasma into a vacuum chamber and imparts a maximum heat flux of 19.5 MW/[Formula: see text] onto [Formula: see text] disks. Heat flux results are calibrated using a combination of thermocouple data as well as multiphysics numerical simulations in COMSOL, which aim to replicate the testing en
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Hei, Li Fu, Fan Xiu Lu, Cheng Ming Li, Wei Zhong Tang, Guang Chao Chen, and Jian Hua Song. "A Review on Mechanical Properties of Freestanding Diamond Films." Advanced Materials Research 490-495 (March 2012): 3059–64. http://dx.doi.org/10.4028/www.scientific.net/amr.490-495.3059.

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As an emerging brand new type of engineering material for a variety of important high technology applications, the deep understanding of the mechanical behavior of freestanding diamond films has become an emergent task of vital importance. Of the many deposition methods dc arc plasma jet has been regarded as the most promising technique for large area high quality and low cost production of freestanding diamond films. In the present paper, recent progress in mechanical properties of freestanding diamond films mainly by high power dc arc plasma jet with rotating arc root and gas recycling is re
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Books on the topic "Arc-jet testing"

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Recent testing of 30kW hydrogen arcjet thrusters. National Aeronautics and Space Administration, 1993.

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Conference papers on the topic "Arc-jet testing"

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White, Susan, and Douglas D. Burleigh. "Thermographic techniques for arc-jet testing." In Optical Engineering and Photonics in Aerospace Sensing, edited by Lee R. Allen. SPIE, 1993. http://dx.doi.org/10.1117/12.141977.

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Burrell, Jack O., and Forrest A. Strobel. "Arc jet testing of a Dynasil dome." In AeroSense '99, edited by Randal W. Tustison. SPIE, 1999. http://dx.doi.org/10.1117/12.354635.

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Risch, Timothy K. "Plasma Arc Jet Testing for Thermal Protection Characterization." In International Conference On Environmental Systems. SAE International, 1994. http://dx.doi.org/10.4271/941371.

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Mazaheri, Ali R., Walter E. Bruce, and Nathaniel J. Mesick. "Methodology for Flight Relevant Arc-Jet Testing of Flexible Thermal Protection Systems." In AIAA Ground Testing Conference. American Institute of Aeronautics and Astronautics, 2013. http://dx.doi.org/10.2514/6.2013-2622.

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Reimer, Thomas, Burkard Esser, and Ali Guelhan. "Arc Jet Testing of CMC Samples with Transpiration Cooling." In 44th AIAA Thermophysics Conference. American Institute of Aeronautics and Astronautics, 2013. http://dx.doi.org/10.2514/6.2013-2904.

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Gokcen, Tahir. "On Characterization of Flow Disturbances in Arc-Jet Testing." In AIAA SCITECH 2024 Forum. American Institute of Aeronautics and Astronautics, 2024. http://dx.doi.org/10.2514/6.2024-1291.

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Perry, Cole. "Arc Jet Ground Testing for Hypersonic Vehicles and Spacecraft." In 2024 Regional Student Conferences, Region I - North East. American Institute of Aeronautics and Astronautics, 2024. http://dx.doi.org/10.2514/6.2024-84645.

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Cinquegrana, Davide, Raffaele Votta, and Eduardo Trifoni. "Rarefaction Effects in NASA arc jet testing at SCIROCCO facility." In 47th AIAA Thermophysics Conference. American Institute of Aeronautics and Astronautics, 2017. http://dx.doi.org/10.2514/6.2017-4450.

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BALTER-PETERSON, ALIZA, FRANK NICHOLS, BRIAN MIFSUD, and WENDELL LOVE. "Arc jet testing in NASA Ames Research Center thermophysics facilities." In AlAA 4th International Aerospace Planes Conference. American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-5041.

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Schairer, Edward, and James Heineck. "Photogrammetric Recession Measurement of Ablative Materials During Arc-Jet Testing." In 45th AIAA Aerospace Sciences Meeting and Exhibit. American Institute of Aeronautics and Astronautics, 2007. http://dx.doi.org/10.2514/6.2007-1158.

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