TY  - JOUR
AB  - THE overall design philosophy of the DAC One‐Elcvcn has already been described in the preceding papers on operating economics and systems—so that this article sets out to extend that information by explaining how the aerodynamic features of the aircraft enable the spscification of this short‐range twin jet to be met.
VL  - 35
IS  - 5
SN  - 0002-2667
DO  - 10.1108/eb033733
UR  - https://doi.org/10.1108/eb033733
AU  - Prior B.J.
PY  - 1963
Y1  - 1963/01/01
TI  - Aerodynamic Design: A Description of the Design Philosophy as It Applies to Performance Requirements, Wings, Flaps, Engine Installations, Tail and Flying Controls
T2  - Aircraft Engineering and Aerospace Technology
PB  - MCB UP Ltd
SP  - 149
EP  - 152
Y2  - 2024/09/20
ER  -