About this scholarly article

2007 22nd International Congress on Instrumentation in Aerospace Simulation Facilities - Development of Pressure-Sensitive Paint Technique in a Supersonic Indraft Wind Tunnel and its Application to a Busemann Biplane by Saito, K.; Nagai, H.; Ogawa, T.; Asai, K. is a scholarly article available to read on EtoBox.

Author

Saito, K.; Nagai, H.; Ogawa, T.; Asai, K.

Publisher

IEEE

Published

2007

Language

EN