Sharp Leading Edge at Hypersonic Flight: Modeling and Flight Measurement

Sharp Leading Edge at Hypersonic Flight: Modeling and Flight Measurement

The octahedral sharp leading edge of the sharp edge flight experiment SHEFEX II is made from carbon fiber reinforced ceramic with a tip radius of

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Bibliographische Detailangaben
Veröffentlicht in:Journal of spacecraft and rockets 2014-09, Vol.51 (5), p.1753-1760
Hauptverfasser: Böhrk, Hannah, Dittert, Christian, Weihs, Hendrik, Thiele, Thomas, Gülhan, Ali
Format: Artikel
Sprache:eng
Schlagworte:
Arc heating
Carbon fiber reinforced ceramics
Carbon fibers
Ceramic fibers
Computer simulation
Fiber reinforced materials
Ground stations
Ground tests
Heat balance method
Heat exchange
Hypersonic flight
Infrared cameras
Leading edges
Reproduction
Rockets
Sharp leading edges
Thermal response
Thermocouples
Transpiration
Wind tunnel testing
Wind tunnels
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Zusammenfassung:The octahedral sharp leading edge of the sharp edge flight experiment SHEFEX II is made from carbon fiber reinforced ceramic with a tip radius of
ISSN:0022-4650
1533-6794
DOI:10.2514/1.A32892