Wind tunnel of National Advisory Committee for Aeronautics is of double-return flow type with 30 by 60-ft open jet at test section; air circulated by two propellers 35 ft 5 in. in diam, located side by side, and each directly connected to 4000-hp slip-ring induction motor; motor-control equipment permits varying speed in 24 steps between 25 and 118 mph; 6-component type balance; calibration and tests.
N.A.C.A. full-scale wind tunnel
Nat Advisory Committee Aeronautics -- Report
1933
10 pages
Report
English
© Metadata Copyright Elsevier B. V. All rights reserved.
The N.A.C.A. full-scale wind tunnel
TIBKAT | 1933
|N.A.C.A. Variable-density wind tunnel
Engineering Index Backfile | 1932
|The N.A.C.A. variable-density wind tunnel
TIBKAT | 1932
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