2-ft 6-in.×2-ft 3-in. tunnel, for speeds ranging from Mach 1.4 to 3.5, completed at Aircraft Research Assn, Bedford; tunnel is driven by 13,750-hp axial compressor which also serves to evacuate ventilated working section of transonic tunnel. (See also Aircraft Eng v 31 n 361 Mar 1959 p 81-3; Engineering v 187 n 4848 Feb 6 1959 p 187-8; Aeroplane v 96 n 2473 Jan 23 1959 p 97-9)
New A.R.A. supersonic wind tunnel
Engineer
Engineer ; 207 , n 5375
1959
179 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
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