A Modified Point-Diffraction Interferometry for Shock Tube Airfoil Testing-Reference-Cited by-同舟云学术

A Modified Point-Diffraction Interferometry for Shock Tube Airfoil Testing

Published:2012-01-09 Issue: Volume: Page:
ISSN:
Container-title:50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
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Author:

Kashitani Masashi¹,Yamaguchi Yutaka¹,Miyazaki Dai¹,Oki Genkai¹

Affiliation:

1. National Defense Academy

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2012-468

Reference19 articles.

1. 1Cook,S.P.,andChokani,N.,QuantitativeResultsfromtheFocusingSchlierenTechnique,AIAApaper93-0630,1993.

2. 2A.H.Shapiro,TheDynamicsandThermodynamicsofCompressibleFluidFlowVol.I,RonaldPress,1953,p.82.

3. 3Brock,N.J.,Chandrasekhara,M.S.,andCarr,L.W.,ARealTimeInterferometry SystemforUnsteadyFlowMeasurements, ICIASF'91 Record,IEEE,Publ.91-CH-3038-8,1991, pp.423 -430.

4. 5Ruetenik, J. R., and Witmer, E. A.: Transient Aerodynamics of Two - DimensionalAirfoils, Part 2 - Interferometric Measurements of Airflow Development about an NACA 65 - 010 Airfoil in Shock - Initiated Subsonic Flow, MIT, WADC TR 54 -368,Part 2, AD151018,1958.

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