Work commenced at site near Bedford, on large tunnel capable of testing models at Mach number of up to 1.3, i.e., 1000 mph at sea level; designed by Aircraft Research Assn for development work on new designs; tunnel speed varied by flaps on guide vanes; models pre-erected on support balance. (see also Engineer v 197 n 5115 Feb 5 1954 p 205-6; Aircraft Production v 16 n 3 Mar 1954 p 11)
Transonic wind tunnel
Engineering
Engineering ; 177 , n 4593
1954
Article (Journal)
English
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Engineering Index Backfile | 1954
Engineering Index Backfile | 1954
AIAA | 1986
|TIBKAT | 1961
|SLUB | 1961
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