A STOL AIRWORTHINESS INVESTIGATION USING A SIMULATION OF AN AUGMENTOR WING TRANSPORT. VOLUME I. SUMMARY OF RESULTS AND AIRWORTHINESS IMPLICATIONS
A simulator study of STOL airworthiness criteria was conducted using a model of an augmentor wing transport. This study covered the approach, flare and landing, go-around, and takeoff phases of flight. The two volumes of this report document the results of that investigation. Volume One summarizes the results and discusses possible implications with regard to airworthiness criteria. The results provide a data base for future STOL airworthiness requirements and a preliminary indication of potential problem areas. The results are also compared to the results from an earlier simulation of the Breguet 941S. Where possible, airworthiness criteria are proposed for consideration.
- Prepared in cooperation with National Aeronautics and Space Administration, Moffett Field, Calif. AMES Research Center. Rept. no. A-5797.
Systems Technology, Incorporated13766 South Hawthorne Boulevard
Hawthorne, CA United States 90250
Ames Research CenterNational Aeronautics and Space Administration
Moffett Field, CA United States 94035
Federal Aviation Administration800 Independence Avenue, SW
Washington, DC United States 20591
- Stapleford, R L
- Heffley, R K
- Hynes, C S
- Scott, B C
- Publication Date: 1974-10
- Pagination: 56 p.
- TRT Terms: Approach; Flight paths; Landing; Lift drag ratio; Simulation; STOL aircraft; Takeoff; Training simulators
- Uncontrolled Terms: Experimental data; Model tests
- Old TRIS Terms: Aircraft landing; Augmentation; Lift to drag ratio; Powered lift; Short takeoff aircraft
- Subject Areas: Aviation; Safety and Human Factors;
- Accession Number: 00090302
- Record Type: Publication
- Source Agency: National Technical Information Service
- Report/Paper Numbers: STI-TR-1047-1 Final Rpt.
- Contract Numbers: NAS2-7926
- Files: NTIS, USDOT
- Created Date: Apr 22 1975 12:00AM