Tests showed that, although slot-tip ailerons did not have lag normally associated with plain spoilers, they were rather slow in developing full amount of rolling moment and therefore imparted sluggish motion to roll of airplane; tests in full scale tunnel showed that drag due to open slot was excessive, but tests in 7 by 10-ft tunnel revealed that drag could be reduced by modifying slot shape.
Wind-tunnel and flight tests of slot-tip ailerons
Nat Advisory Committee Aeronautics -- Report
1937
25 pages
Bibliography
Report
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Wind-tunnel and flight tests of slot-tip ailerons
Engineering Index Backfile | 1937
|Wind-tunnel and flight tests of slot-tip ailerons
Engineering Index Backfile | 1937
|Wind-Tunnel and Flight Tests of Slot-lip Ailerons
NTRS | 1937
|Wind-tunnel and flight tests of slot-lip ailerons
TIBKAT | 1937
|Wind tunnel tests on Junker type ailerons
SLUB | 1934
|