DLR PSP system: Intensity and lifetime measurements

ICIASF Record, International Congress on Instrumentation in Aerospace Simulation Facilities

Volumn 1997, Issue , 1997, Pages 46-55

  Engler, R H ^a   Klein, Chr ^a  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

CALIBRATION; COMPUTER APPLICATIONS; COMPUTER HARDWARE; COMPUTER SIMULATION; COMPUTER SOFTWARE; LASERS; LIGHTING; OPTICAL VARIABLES MEASUREMENT; PAINT; PRESSURE MEASUREMENT; WIND TUNNELS;

PRESSURE SENSITIVE PAINT; TRANSONIC WIND TUNNEL GOETTINGEN;

OPTICAL INSTRUMENTS;

EID: 0031353544     PISSN: 07302010     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Article

References (8)

1. J.F. Donovan, M.J. Morris, A. Pal, M.E. Benne, R.C. Crites, "Data Analysis Techniques for Pressure- and Temperature-Sensitive Paint", 31st Aerospace Sciences Meeting & Exhibit, Reno, NV, AIAA Paper 93-0176, Jan. 1993
2. V. Borovoy, A. Bykov, V. Mosharov, A. Orlov, V. Radchenko, S. Fonov, "Pressure Sensitive Paint Application in Shock Wind Tunnel", 16th ICIASF Congress, Dayton, Ohio, July 1995
3. A. Bykov, S. Fonov, A. Kishalov, A. Orlov, S. Ostroukhov, V. Radchenko, "Application of Luminescent Pressure Technology to Propellers", Preprint No. 99, TsA-GI, Moscow 1995
4. R.H. Engler, K. Hartmann, B. Schulze, "Aerodynamic Assessment of an Optical Pressure Measurement System (OPMS) by Comparison with Conventional Pressure Measurements in High Speed Wind Tunnel", 14th ICIASF Congress, Rockville, MD, October 1991
5. R.H. Engler, "Futher Developments of Pressure Sensitive Paint for Non Flat Models in Steady Transonic Flow and Unsteady Conditions", 16th ICIASF Congress, Dayton, Ohio, July 1995
6. J.H. Bell, B.G. McLachlan, "Image Registration for Luminescent Paint Sensors", 31st Aerospace Sciences Meeting & Exhibit, Reno, NV, AIAA Paper 93-0178, Jan. 1993
7. Y. Le Sant, M.C. Merienne, "An Image Resection Method Applied to Mapping Techniques", 16th ICIASF Congress, Dayton, Ohio, July 1995
8. M.E. Sellers, J.A. Brill, "Demonstration Test of Pressure Sensitive Paint in the AEDC 16-ft Transonic Wind Tunnel Using the TST Model", 18th AIAA Aerospace Ground Testing Conference, Colorado Springs, CO, AIAA Paper 94-2231, June 1994