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Simulation of decelerating landing approaches on an externally blown flap stol transport airplane
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Deal, P. L. Nguyen, L. T. Grantham, W. D. |
| Copyright Year | 1974 |
| Description | A fixed-base simulator program was conducted to define the problems and methods for solution associated with performing decelerating landing approaches on a representative STOL transport having a high wing and equipped with an external-flow jet flap in combination with four high-bypass-ratio fan-jet engines. Real-time digital simulation techniques were used. The computer was programed with equations of motion for six degrees of freedom and the aerodynamic inputs were based on measured wind-tunnel data. The pilot's task was to capture the localizer and the glide slope and to maintain them as closely as possible while decelerating from an initial airspeed of 140 knots to a final airspeed of 75 knots, while under IFR conditions. |
| File Size | 16562236 |
| Page Count | 51 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740013545 |
| Archival Resource Key | ark:/13960/t04z02g75 |
| Language | English |
| Publisher Date | 1974-05-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Externally Blown Flaps Aircraft Landing Transport Aircraft Aircraft Performance Short Takeoff Aircraft Aerodynamic Characteristics Lift Augmentation Flight Simulation Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
