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タイトルDevelopment of a Large Field of View Shadowgraph System for a 16 Ft. Transonic Wind Tunnel
本文(外部サイト)http://hdl.handle.net/2060/20000108883
著者(英)Goodman, Wesley L.; Talley, Michael A.; Jones, Stephen B.
著者所属(英)NASA Langley Research Center
発行日2000-09-01
言語eng
内容記述A large field of view shadowgraph flow visualization system for the Langley 16 ft. Transonic Tunnel (16 ft.TT) has been developed to provide fast, low cost, aerodynamic design concept evaluation capability to support the development of the next generation of commercial and military aircraft and space launch vehicles. Key features of the 16 ft. TT shadowgraph system are: (1) high resolution (1280 X 1024) digital snap shots and sequences; (2) video recording of shadowgraph at 30 frames per second; (3) pan, tilt, & zoom to find and observe flow features; (4) one microsecond flash for freeze frame images; (5) large field of view approximately 12 X 6 ft; and (6) a low maintenance, high signal/noise ratio, retro-reflective screen to allow shadowgraph imaging while test section lights are on.
NASA分類Instrumentation and Photography
レポートNONASA/TM-2000-210311
L-18009
NAS 1.15:210311
権利No Copyright
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/93902


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