Study on Effects of Operation Gas for Shock Tube Airfoil Flows with Point-Diffraction Interferometer-Reference-Cited by-同舟云学术

Study on Effects of Operation Gas for Shock Tube Airfoil Flows with Point-Diffraction Interferometer

Published:2011 Issue:685 Volume:59 Page:34-41
ISSN:1344-6460
Container-title:JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:ja
Short-container-title:JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES

Author:

KASHITANI Masashi,YAMAGUCHI Yutaka,OKI Genkai

Publisher

Japan Society for Aeronautical and Space Sciences

Link

https://www.jstage.jst.go.jp/article/jjsass/59/685/59_685_34/_pdf

Reference27 articles.

1. 1) Ruetenik, J. R. and Witmer, E. A.: Transient Aerodynamics of Two-Dimensional Airfoils, 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, AD 151018, 1958.

2. 2) Takayama, K.: Application of Holographic Interferometry to Shock Wave Research, Proc. 12th ISST & W, 1980, pp. 174-180.

3. 3) Smartt, R. N. and Steel, W. H.: Theory and Application of Point-Diffraction Interferometers, Jpn. J. Appl. Phys., 14, Suppl. 14-1 (1975), pp. 351-356.

4. 4) Smartt, R. N. and Strong, J.: Point-Diffraction Interferometer, J. Opt. Soc. Am., 62 (1972), p. 737.

5. 5) Carr, L. W., Chandrasekhara, M. S., Ahmed, S. and Brock, N.: A Study of Dynamic Stall Using Real-Time Interferometry, AIAA Paper 91-0007, 1991.

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. A Modified Point-Diffraction Interferometry for Shock Tube Airfoil Testing;50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2012-01-09