Powerplant: Fuel System

Abstract

THE need to carry sufficient fuel in the smallest possible space and with the lowest possible weight dictated the use of integral fuel tanks in both the wing and the fuselage, despite the recognised difficulty of scaling tanks of conventional aircraft construction with complex shapes.

Citation

(1970), "Powerplant: Fuel System", Aircraft Engineering and Aerospace Technology, Vol. 42 No. 1, pp. 28-31. https://doi.org/10.1108/eb034593