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Deep stall characteristics of mu-300
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Hanai, T. |
| Copyright Year | 1986 |
| Description | The deep stall characteristics of the MU-300 Diamond aircraft are described. The MU-300 obtained type certification from the FAA in 1981, and from Canada, West Germany, and England in 1983. The aircraft has achieved a high angle of attack. The aerodynamic design, structural dimensions, and flight tests of the MU-300 are described. |
| File Size | 550789 |
| Page Count | 14 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19870004885 |
| Archival Resource Key | ark:/13960/t2v45mb09 |
| Language | English |
| Publisher Date | 1986-09-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Flight Tests Flight Characteristics Civil Aviation Wind Tunnel Tests Aircraft Design Angle of Attack Aerodynamic Stalling Accidents Dynamic Pressure Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
