TECHNICAL PAPERS

Determination of the Operational Environment of the Propeller Blades on Beech 1900D Aircraft

Date Published: 2008-08-19
Paper Number: 2008-01-2226
DOI: 10.4271/2008-01-2226

Citation:

Dorfling, J., Kliment, L., Rokhsaz, K., DeFiore, T. et al., "Determination of the Operational Environment of the Propeller Blades on Beech 1900D Aircraft," SAE Technical Paper 2008-01-2226, 2008, doi:10.4271/2008-01-2226.

Author(s):


J. Dorfling - Wichita State Univ.
L. K. Kliment - Wichita State Univ.
K. Rokhsaz - Wichita State Univ.
T. DeFiore - FAA William J. Hughes Technical Center
C. Nguyen - FAA William J. Hughes Technical Center
J. E. Turnberg - FAA Engine and Propeller Directorate

Abstract:

Data obtained from digital flight data recorders are used to assess the actual operational environment of propellers on a fleet of Beech 1900D aircraft in commuter role. Information is given on various aerodynamic parameters as well as those pertaining to engine and propeller usage. The takeoff rotation has been identified as the most demanding phase of flight in terms of unsteady loads exerted on the propeller blades. Special attention is paid to ground operations.

File Size: 393K

Product Status: In Stock

See papers presented at Wichita Aviation Technology Congress & Exhibition, August 2008, Wichita, KS, USA, Session: Propulsion

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