Some Considerations Regarding the Application of the Supersonic Area Rule to the Design of Airplane Fuselages
1956
27 pages
Report
Keine Angabe
Englisch
Aircraft , Aircraft design , Fuselage , Supersonic aircraft , Wave drag , Area , Body , Combination , Design , Drag , Rule , Speed , Supersonic , Surface , Tail , Wave , Wing
Shaping of airplane fuselages for minimum drag
AIAA | 1987
|Tests on airplane fuselages, floats and hulls
NTRS | 1927
|