Numerical-experimental correlation of stagnation point heat flux in high enthalpy hypersonic Wind Tunnel

A Collection of Technical Papers - 13th AIAA/CIRA International Space Planes and Hypersonic Systems and Technologies Conference

Volumn 1, Issue , 2005, Pages 715-726

  De Filippis, F ^a   Savino, R ^b,c   Martucci, A ^b,c  

^a ITALIAN AEROSPACE RESEARCH CENTER   (Italy)

^b Depts of Space Science and Engineering   (Italy)

^c UNIVERSITY OF NAPLES FEDERICO II   (Italy)

Author keywords

[No Author keywords available]

Indexed keywords

GAUGE CALORIMETER; HYPERSONIC PLASMA; PLASMA WIND TUNNEL; PRESSURE PORT;

CALORIMETERS; COMPUTER SIMULATION; CORRELATION METHODS; ENTHALPY; HEAT FLUX; WIND TUNNELS;

HYPERSONIC AERODYNAMICS;

EID: 29044436578     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (10)

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