Tests to determine change in slipstream effects and rudder control due to variations in shape and vertical location of rudder and fin; vertical tail surfaces tested on DH-4B model; results given by graphs of coefficients; high-aspect-ration gives best rudder control at expense of somewhat greater rudder angle.
Wind tunnel tests of DH-4B model fitted with various fins and rudders
Air Corps Information Cir
Air Corps Information Circular ; 7 , n 603
1927
11 pages
17 Figs.
Article (Journal)
English
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Engineering Index Backfile | 1902
|Engineering Index Backfile | 1929
|Engineering Index Backfile | 1929
|British Library Conference Proceedings | 2004
|Engineering Index Backfile | 1917
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