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 Engineering v 187 n 4848 Feb 6 1959 p 187-8; Engineer v 207 n 5375 Jan 30 1959 p 179; Aeroplane v 96 n 2473 Jan 23 1959 p 97-99)
New A.R.A. supersonic wind tunnel
Aircraft Eng
Aircraft Engineering ; 31 , n 361
1959
3 pages
Aufsatz (Zeitschrift)
Englisch
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New A.R.A. supersonic wind tunnel
Engineering Index Backfile | 1959
New A.R.A. supersonic wind tunnel
Engineering Index Backfile | 1959
New A.R.A. supersonic wind tunnel
Engineering Index Backfile | 1959
The New A.R.A. Supersonic Wind Tunnel
Emerald Group Publishing | 1959
A.R.A. holds ninth meeting and fifth exhibit
Engineering Index Backfile | 1928