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Boron/aluminum fan blades for scar engines
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Stabrylla, R. G. Carlson, R. G. |
| Copyright Year | 1977 |
| Description | Processing procedures were developed to enhance boron/aluminum bond behavior and foreign object damage (FOD) tolerance. Design and analysis indicated that the J101 Stage 1 fan blade meets the required frequencies without a midspan shroud. The fabricability of full size J101 blades was assessed, while six blades were fabricated and finished machined. |
| File Size | 5998988 |
| Page Count | 137 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19770019191 |
| Archival Resource Key | ark:/13960/t9j43jq37 |
| Language | English |
| Publisher Date | 1977-06-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Propeller Blades Aluminum Boron Composites Supersonic Aircraft Propeller Fans Cruising Flight Impact Tests Composite Structures Impact Tolerances 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 |