Tests with Junkers (D 1010) A. 35 type monoplane equipped with sliding weight and water tank to shift position of center of pressure at will; curves show relations between static pressures, elevator settings and throttle positions; computation of required thrust for level flight for each throttle setting with polar of model test as basis; blanketing effect of propeller. From 1930 Yearbook of Deutscher Versuchsanstalt fuer Luftfahrt. (see also Jahrbuch 1930 der Deutschen Versuchsanstalt fuer Luftfahrt, E. V., pp. 49-53, 16 figs.)
Flight tests for the determination of static longitudinal stability
Nat. Advisory Committee Aeronautics -- Tech. Memo
1930
11 pages
16 Figs. on Supp. plates
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Aeroelastic Characteristics and Static Stability of Hang Gliders in Longitudinal Flight
British Library Conference Proceedings | 1994
|