TY - GEN
T1 - Surface pressure measurements over a free flight object in a ballistic range facility using two-color pressure-sensitive paint
AU - Kurihara, Daiki
AU - Caucherty, Steven
AU - Gonzales, Joseph
AU - Sakaue, Hirotaka
AU - Kiritani, Hideki
AU - Fujita, Koji
AU - Nagai, Hiroki
N1 - Funding Information:
This project was supported by Discretionary Collaborative Research at Institute of Fluid Science (IFS), Tohoku University. Notre Dame authors would like to thank IFS for providing the opportunity to create an international collaboration between Notre Dame and IFS through this funding. The authors would like to acknowledge Photron for their high-speed color camera support.
Publisher Copyright:
© 2020, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2020
Y1 - 2020
N2 - The present study focuses on the challenges of capturing surface pressure data on a free-flight object in a ballistic range facility. There are four main challenges: (1) shooting an aerodynamic model in a ballistic range; (2) capturing the free-flight trajectory; (3) capturing luminescent images of the object during the flight; and (4) obtaining the surface pressure distribution from the luminescent images. Prior work has been successful with the first two challenges; this study will focus on methods to overcome the third and fourth challenges using two-color pressure-sensitive paint (PSP). Using two-color PSP allows the implementation of the motion-capturing method, using a reference signal to fix the position of the signal from the PSP. Tests over the course of this campaign have shown an improvement in image quality by reducing image blur; this work presents the results of a test campaign in Tohoku University’s ballistic range, showing that PSP can be used to capture the pressure distribution over a test article in free-flight.
AB - The present study focuses on the challenges of capturing surface pressure data on a free-flight object in a ballistic range facility. There are four main challenges: (1) shooting an aerodynamic model in a ballistic range; (2) capturing the free-flight trajectory; (3) capturing luminescent images of the object during the flight; and (4) obtaining the surface pressure distribution from the luminescent images. Prior work has been successful with the first two challenges; this study will focus on methods to overcome the third and fourth challenges using two-color pressure-sensitive paint (PSP). Using two-color PSP allows the implementation of the motion-capturing method, using a reference signal to fix the position of the signal from the PSP. Tests over the course of this campaign have shown an improvement in image quality by reducing image blur; this work presents the results of a test campaign in Tohoku University’s ballistic range, showing that PSP can be used to capture the pressure distribution over a test article in free-flight.
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U2 - 10.2514/6.2020-0123
DO - 10.2514/6.2020-0123
M3 - Conference contribution
AN - SCOPUS:85091940032
SN - 9781624105951
T3 - AIAA Scitech 2020 Forum
BT - AIAA Scitech 2020 Forum
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Scitech Forum, 2020
Y2 - 6 January 2020 through 10 January 2020
ER -