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Problems in propulsion system integration
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Henderson, W. P. Runckel, J. F. |
| Copyright Year | 1975 |
| Description | Jet engine components are considered that influence propulsion system integration on the airframe and related aircraft drag areas. Emphasis is placed on high Mach number inlet geometries, boattailed nozzle configurations, propulsive wing installation, wing surface blowing lift, fuselage mounted nacelles, and thrust reversal. |
| File Size | 4258997 |
| Page Count | 22 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19760003937 |
| Archival Resource Key | ark:/13960/t8md3q56p |
| Language | English |
| Publisher Date | 1975-01-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Engine Design Drag Reduction Body-wing Configurations Airframes Engine Inlets Aircraft Configurations Propulsion System Configurations Jet Engines Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |