Loading...
Please wait, while we are loading the content...
Similar Documents
Theoretical flow characteristics of inlets for tilting-nacelle vtol aircraft
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Boles, M. A. Stockman, N. O. Luidens, R. W. |
| Copyright Year | 1978 |
| Description | The results of a theoretical investigation of geometric variables for lift-cruise-fan, tilting nacelle inlets operating at high incidence angles are presented. These geometric variables are investigated for their effects on surface static to free stream pressure ratio, and the separation parameters of maximum to diffuser exit surface velocity ratio and maximum surface Mach number for low speed operating conditions. The geometric parameters varied were the internal lip contraction ratio, external forebody to diffuser exit diameter ratio external forebody length to diameter ratio and internal lip major to minor axis ratio. |
| File Size | 1153809 |
| Page Count | 33 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19780013171 |
| Archival Resource Key | ark:/13960/t40s4k69d |
| Language | English |
| Publisher Date | 1978-04-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Attitude Inclination Flow Characteristics Inlet Flow Nacelles Contraction Mach Number Incidence Vertical Takeoff Aircraft Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |