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Nacelle drag reduction: an analytically-guided experimental program
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Smetana, F. O. |
| Copyright Year | 1975 |
| Description | 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. |
| File Size | 223564 |
| Page Count | 5 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19760003928 |
| Archival Resource Key | ark:/13960/t6q00051p |
| Language | English |
| Publisher Date | 1975-01-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Drag Reduction Nacelles Computerized Simulation Estimates Interference Drag Prediction Analysis Techniques Forebodies Wing-fuselage Stores Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |