Loading...
Please wait, while we are loading the content...
Similar Documents
An analysis of prop-fan/airframe aerodynamic integration
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Clay, C. W. Watson, C. F. Boctor, M. L. |
| Copyright Year | 1978 |
| Description | An approach to aerodynamic integration of turboprops and airframes, with emphasis placed upon wing mounted installations is addressed. Potential flow analytical techniques were employed to study aerodynamic integration of the prop fan propulsion concept with advanced, subsonic, commercial transport airframes. Three basic configurations were defined and analyzed: wing mounted prop fan at a cruise Mach number of 0.8, wing mounted prop fan in a low speed configuration, and aft mounted prop fan at a cruise Mach number of 0.8. |
| File Size | 15927601 |
| Page Count | 78 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19840011213 |
| Archival Resource Key | ark:/13960/t1sf7k90d |
| Language | English |
| Publisher Date | 1978-10-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Turbulent Wakes Airframes Prop-fan Technology Slipstreams Wind Tunnel Models Wing Profiles Aerodynamic Characteristics Swirling Potential Flow Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |