Fatigue analysis of the Beech Super King Air empennage was performed in compliance with the Australian and British certification requirements. The empennage fatigue loads for this analysis were evaluated with the use of an engineering flight simulator. The empennage balance, maneuvering, and gust loads for both the horizontal and vertical tail were determined for various flight conditions. These loads were used for analytical prediction of safe life of the empennage structure.
Evaluation of Empennage Fatigue Loads for the Beech Super King Air Using a Flight Simulator
Sae Technical Papers
National Business Aircraft Meeting and Engineering Display ; 1977
01.02.1977
Aufsatz (Konferenz)
Englisch
General Aviation Aircraft Empennage Flight Loads
British Library Conference Proceedings | 1999
|General Aviation Aircraft Empennage Flight Loads
SAE Technical Papers | 1999
|British Library Online Contents | 2008
|DEVELOPMENT OF COMMUTER AIRCRAFT EMPENNAGE LOADS SPRCTRUM
British Library Online Contents | 2003
|