Development of Air Force Flight Safety Models. Volume 16. Feasibility of Adapting Model to Rotary Wing Aircraft; Example: UH-1N
Development of Air Force Flight Safety Models. Volume 16. Feasibility of Adapting Model to Rotary Wing Aircraft; Example: UH-1N
The feasibility of applying the Flight Safety Prediction Technique to rotary wing aircraft is demonstrated through its application to the UH-1N helicopter. A complete safety model, compatible with the computer program used for a fixed wing aircraft, is presented. (Author)
Document information
Development of Air Force Flight Safety Models. Volume 16. Feasibility of Adapting Model to Rotary Wing Aircraft; Example: UH-1N
1976
84 pages
Report
No indication
English
Aeronautics , Aircraft , Air Transportation , Aviation safety , Mathematical models , Airworthiness , Helicopters , Aircraft maintenance , Safety equipment , Aircraft equipment , Failure , Weighting functions , Probability , Mathematical prediction , Adaptation , Computer applications , Cost analysis , UH-1N aircraft , H-1 aircraft
Similar titles
Rotary wing aircraft development
| Engineering Index Backfile | 1954
Rotary wing aircraft development
| Engineering Index Backfile | 1954