Lift distribution produced by aileron deflections for rectangular wing on straight flight previously determined on theoretical principles for certain case, and air forces and moments produced by ailerons derived; approximate values deduced from former results for use in calculating acting forces and moments for all cases; results expressed by non-dimensional coefficients represented in diagrams. (see also Nat. Advisory Committee for Aeronautics -- Tech. Memo., no. 488, Nov. 1928, 15 pp., 10 figs. on supp. pp)
Determination of air forces and moments produced by ailerons of airplane
Bestimmung der durch die Querruder eines Tragfluegels erzeugten Luftkraefte und Momente
Zeitschrift fur Flugtechnik und Motorluftschiffahrt ; 19 , n 13 ; p 289-293
1928
5 pages
10 Figs.
Article (Journal)
German
© Metadata Copyright Elsevier B. V. All rights reserved.
Determination of air forces and moments produced by ailerons of airplane
Engineering Index Backfile | 1928
|Rolling, yawing, and hinge moments produced by rectangular ailerons
Engineering Index Backfile | 1933
|Theoretical investigation of rolling oscillations of airplane with ailerons free
Engineering Index Backfile | 1946
|Forces and moments on airplane engine mounts
Engineering Index Backfile | 1936
|Engineering Index Backfile | 1934
|