360° PSP measurements in transonic flow

ICIASF Record, International Congress on Instrumentation in Aerospace Simulation Facilities

Volumn , Issue , 2001, Pages 149-158

  Engler, R H ^a   Klein, C ^a   Merlo, E ^a   Van Amerom, P ^a  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT MODELS; CAMERAS; CHARGE COUPLED DEVICES; COMPUTER SOFTWARE; ERROR ANALYSIS; PRESSURE DISTRIBUTION; PRESSURE MEASUREMENT; WIND TUNNELS;

WIND TUNNEL MEASUREMENTS;

TRANSONIC FLOW;

EID: 0035158698     PISSN: 07302010     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (11)

1. New optical pressure measurement system
2. Aerodynamic assessment of an optical pressure measurement system (OPMS) by comparison with conventional pressure measurements in a high speed wind tunnel
3. Set of luminescence pressure sensors for aerospace research
4. Aero-dynamic applications of pressure sensitive paint
5. Image registration for luminescent paint sensors
6. Surface pressure field mapping using luminescent coatings
7. Further developments of pressure sensitive paint for non flat models in stead transonic flow and unsteady conditions
8. First results using the new DLR PSP system - Intensity and lifetime measurements
9. On the effects of reflected light in luminescent paint measurements
10. Application of pressure sensitive paint for determining aerodynamic loads on a scale of the F-16C