Tests of Dynamic Model in NACA Tank No. 1 to Determine Effect of Length of Afterbody, Angle of Afterbody Keel, Gross Load, and Pointed Step on Landing and Planing Stability. (Advance Restricted Report)
Tests of dynamic model in NACA tank No. 1 to determine effect of length of afterbody, angle of afterbody keel, gross load, and pointed step on landing and planing stability
Nat Advisory Committee Aeronautics -- Wartime Report
1943
11 pages
17 Supp plates
Report
Englisch
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Effect of streamlining afterbody of NACA cowling
Engineering Index Backfile | 1939
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