Tests of parachutes on six models of typical fighter and trainer airplanes. (Originally issued as Advance Restricted Report L5G19a Mar 1946)
Comparison of tail and wing-tip spin-recovery parachutes as determined by tests in Langley 20-foot freespinning tunnel, R
Nat Advisory Committee Aeronautics -- Wartime Report
1946
25 pages
27 Supp plates
Report
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Wing parachutes for recovery from the spin
TIBKAT | 1954
|Tests of full-scale horizontal tail surface in Langley 16-foot high-speed tunnel
Engineering Index Backfile | 1946
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