Experimental investigation of shock wave / boundary layer interactions over an artificially heated model in hypersonic flow

8th AIAA International Space Planes and Hypersonic Systems and Technologies Conference

Volumn , Issue , 1998, Pages 330-339

  Scortecci, Fabrizio ^a   Paganucci, Fabrizio ^a   D’Agostinof, Luca ^b  

^a Centrospazio CPR   (Italy)

^b UNIVERSITY OF PISA   (Italy)

Author keywords

[No Author keywords available]

Indexed keywords

ENTHALPY; HEAT FLUX; HYPERSONIC FLOW; WIND TUNNELS;

EXPERIMENTAL INVESTIGATIONS; EXPERIMENTAL TEST; HIGH-TEMPERATURE RADIATORS; RELAXATION PHENOMENA; SHOCK-WAVE/BOUNDARY LAYER INTERACTIONS; THIN-FILM GAUGES; TOTAL TEMPERATURES; WALL TEMPERATURES;

SHOCK WAVES;

EID: 84983120196     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-1571     Document Type: Conference Paper

References (4)

1. Scortecci, F., Paganucci, F., Oest, H., "Hot Experimental Testing for Shock-Wave/Boundary-Layer Interaction, Final Report", FESTIP/01/96, Centrospazio, Pisa, 1996
2. Scortecci, F., Paganucci, F., d'Agostino, L., Andrenucci, M., "A New Hypersonic High Enthalpy Wind Tunnel", 33rd Joint Propulsion Conference, AIAA 97-3017, Seattle, 1997
3. rd Joint Propulsion Conference, AIAA 97-3016, Seattle, 1997
4. Scortecci, F., Paganucci, F., Biagioni, L., Borrelli, S., Marini, M., "Disegno dell'ugello per una galleria ipersonica ad alta entalpia", XIII Congresso Nazionale AIDAA, Napoli, 1997