Document Type
Report
Publication Date
9-1990
Abstract
The classical equations for determining the maximum range of aircraft with propeller and jet propulsion systems are reviewed, along with previous work conducted to determine the optimal division of aircraft volume between fuselage and wing components. That the jet powered flying wing configuration produces optimal range only for limited geometries is confirmed. The optimal range of aircraft employing high bypass jet engines is explored, and found to lead to a broader range of design parameters for which the flying wing design produces maximum range than is the case when a pure jet system is used.
Recommended Citation
Torkik, P. J. (1990). On the Maximum Range of Flying Wings. AFIT Report AFIT/EN-TR-90-07. https://scholar.afit.edu/docs/149
DTIC Accession Number
ADA229487
Document / Report Number
AFIT/EN-TR-90-07