Measuring Global Surface Pressures on a Circulation Control Concept Using Pressure Sensitive Paint

[1]  William L. Weaver,et al.  Pressure-sensitive-paint measurements in a large-scale commercial-engine test stand , 1999, ICIASF 99. 18th International Congress on Instrumentation in Aerospace Simulation Facilities. Record (Cat. No.99CH37025).

[2]  John Abbitt,et al.  Pressure Sensitive Paint response to a step pressure change , 1995 .

[3]  V. Altuzar,et al.  Atmospheric pollution profiles in Mexico City in two different seasons , 2003 .

[4]  Odis C. Pendergraft,et al.  Flow Visualization at Cryogenic Conditions Using a Modified Pressure Sensitive Paint Approach , 2005 .

[5]  J. Bell,et al.  Pressure-sensitive paint in aerodynamic testing , 1993 .

[6]  A. Neal Watkins,et al.  Results From a Pressure Sensitive Paint Test Conducted at the National Transonic Facility on Test 197: The Common Research Model , 2011 .

[7]  É. Germain,et al.  The Development and Application of Optical Measurement Techniques for High Reynolds Number Testing in Cryogenic Environment , 2005 .

[8]  Hiroshi Kanda,et al.  Surface pressure measurement in a cryogenic wind tunnel by using luminescent coating , 1997, ICIASF'97 Record. International Congress on Instrumentation in Aerospace Simulation Facilities.

[9]  Martin Morris,et al.  Aerodynamic measurements based on photoluminescence , 1993 .

[10]  J. Bell,et al.  Surface Pressure Measurements Using Luminescent Coatings , 2003 .

[11]  Martin Morris,et al.  Use of pressure-sensitive paints in low-speed flows , 1995, ICIASF '95 Record. International Congress on Instrumentation in Aerospace Simulation Facilities.

[12]  T. Mark Walter,et al.  A Comparison of Pressure Sensitive Paint (PSP) Techniques for Aerodynamic Testing at Slow Velocities , 2002 .

[13]  Bruce Carroll,et al.  Frequency response of pressure sensitive paints , 1996 .

[14]  J. Callis,et al.  Luminescent barometry in wind tunnels , 1990 .

[15]  Bryan Campbell,et al.  Temperature- and Pressure-Sensitive Luminescent Paints in Aerodynamics , 1997 .

[16]  J. Lakowicz Principles of fluorescence spectroscopy , 1983 .

[17]  Hiroshi Kanda,et al.  Detection of Boundary-Layer Transition in a Cryogenic Wind Tunnel by Using Luminescent Paint , 1996 .

[18]  Eiji Isobe,et al.  Poly[1-(trimethylsilyl)-1-propyne]: a new high polymer synthesized with transition-metal catalysts and characterized by extremely high gas permeability , 1983 .

[19]  Keisuke Asai,et al.  Novel pressure-sensitive paint for cryogenic and unsteady wind tunnel testing , 2000 .