Modifications are proposed to standard estimating procedures, as well as the BODY computer program, which predict that the drag of two nacelles will equal the drag of the fuselage. A preliminary computer analysis that considers increased dimensions for the nacelle forebody so that the noise is relatively less blunt indicates a reduction in form drag much greater than the increase in skin friction drag attributable to increased surface area.
Nacelle drag reduction: An analytically-guided experimental program
01.01.1975
Aufsatz (Konferenz)
Keine Angabe
Englisch
| NTRS | 1979
Experimental and Numerical Investigation on Liplets for Wing/Nacelle Interference Drag Reduction
| British Library Conference Proceedings | 1994
Experimental and Numerical Investigation on Liplets for Wing/Nacelle Interference Drag Reduction
| British Library Online Contents | 1994
Overview of external Nacelle drag and interference drag
| NTRS | 1975