Subsonic transport aircraft flying profile in abnormal flight conditions /
Aircraft performance in crash Simulation (APICS) method has been developed for reconstructing aircraft flight profiles. Analysis is performed using nonlinear six degrees fo freedom equations of motion, PC-based, fixed stick simulation to establish the relative performance degradation resulting from...
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Sekudai : UTM,
1994
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| _version_ | 1796700792811421696 |
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| author | 225339 Sallehuddin Muhamad |
| author_facet | 225339 Sallehuddin Muhamad |
| author_sort | 225339 Sallehuddin Muhamad |
| collection | OCEAN |
| description | Aircraft performance in crash Simulation (APICS) method has been developed for reconstructing aircraft flight profiles. Analysis is performed using nonlinear six degrees fo freedom equations of motion, PC-based, fixed stick simulation to establish the relative performance degradation resulting from several factors that are candidate causes or contributing factors to an accident. Nine scenarios are considered - heavy rain, wind shear, icing condition,engine failure, control system failure, center of gravity movement, take-off with flap retracted, early rotation during take-off and entering a spin. Results achieved are consistent to theoretical values. The method is also capable to verify the probable cause of an air crash. this capability is illustrated in confirming the L-10II crash in 1985 dn the B727 crash in 1988, both crashes occured at Dallas-Fort Worth International Airport. |
| first_indexed | 2024-03-05T02:05:24Z |
| format | |
| id | KOHA-OAI-TEST:271991 |
| institution | Universiti Teknologi Malaysia - OCEAN |
| last_indexed | 2024-03-05T02:05:24Z |
| publishDate | 1994 |
| publisher | Sekudai : UTM, |
| record_format | dspace |
| spelling | KOHA-OAI-TEST:2719912020-12-19T17:08:43ZSubsonic transport aircraft flying profile in abnormal flight conditions / 225339 Sallehuddin Muhamad Sekudai : UTM,1994Aircraft performance in crash Simulation (APICS) method has been developed for reconstructing aircraft flight profiles. Analysis is performed using nonlinear six degrees fo freedom equations of motion, PC-based, fixed stick simulation to establish the relative performance degradation resulting from several factors that are candidate causes or contributing factors to an accident. Nine scenarios are considered - heavy rain, wind shear, icing condition,engine failure, control system failure, center of gravity movement, take-off with flap retracted, early rotation during take-off and entering a spin. Results achieved are consistent to theoretical values. The method is also capable to verify the probable cause of an air crash. this capability is illustrated in confirming the L-10II crash in 1985 dn the B727 crash in 1988, both crashes occured at Dallas-Fort Worth International Airport.Thesis (MSc of Mechanical Engineering) - Universiti Teknologi Malaysia, 1994Aircraft performance in crash Simulation (APICS) method has been developed for reconstructing aircraft flight profiles. Analysis is performed using nonlinear six degrees fo freedom equations of motion, PC-based, fixed stick simulation to establish the relative performance degradation resulting from several factors that are candidate causes or contributing factors to an accident. Nine scenarios are considered - heavy rain, wind shear, icing condition,engine failure, control system failure, center of gravity movement, take-off with flap retracted, early rotation during take-off and entering a spin. Results achieved are consistent to theoretical values. The method is also capable to verify the probable cause of an air crash. this capability is illustrated in confirming the L-10II crash in 1985 dn the B727 crash in 1988, both crashes occured at Dallas-Fort Worth International Airport.19FEMELStability of airplanesFlight control |
| spellingShingle | Stability of airplanes Flight control 225339 Sallehuddin Muhamad Subsonic transport aircraft flying profile in abnormal flight conditions / |
| title | Subsonic transport aircraft flying profile in abnormal flight conditions / |
| title_full | Subsonic transport aircraft flying profile in abnormal flight conditions / |
| title_fullStr | Subsonic transport aircraft flying profile in abnormal flight conditions / |
| title_full_unstemmed | Subsonic transport aircraft flying profile in abnormal flight conditions / |
| title_short | Subsonic transport aircraft flying profile in abnormal flight conditions / |
| title_sort | subsonic transport aircraft flying profile in abnormal flight conditions |
| topic | Stability of airplanes Flight control |
| work_keys_str_mv | AT 225339sallehuddinmuhamad subsonictransportaircraftflyingprofileinabnormalflightconditions |