Preliminary Study on Diaphragmless Shock Tube for Transonic Airfoil Testing with PDI-Reference-Cited by-同舟云学术

Preliminary Study on Diaphragmless Shock Tube for Transonic Airfoil Testing with PDI

Published:2010-01-04 Issue: Volume: Page:
ISSN:
Container-title:48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
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Author:

Kashitani Masashi¹,Yamaguchi Yutaka¹,Oki Genkai¹,Kitano Hideki¹,Esashi Satoru¹

Affiliation:

1. National Defense Academy

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-744

Reference15 articles.

1. M. Kashitani, Y. Yamaguchi, E. Sunahara, and H. Kitano, Preliminary Study on Sidewall Boundary Layers in Transonic ShockTubeAirfoilTesting,AIAApaper2008-0850,(2008).

2. Airfoil Flow Visualization and Pressure Measurements in High-Reynolds-Number Transonic Flow

3. 4T. Otomo, T. Kuribayashi. and K. Takayama, The Characteristics of 100 mm×180 mm Diaphragmless Shock Tube after Improvement,2002 ShockWave Symposium,(2003)pp.7-8.(In Japanese)

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