Ibrahim, K (2003) Selecting fuel fraction, propeller diameter and fuselage length for military propeller trainers 13;. In: 21st AIAA Applied Aerodynamics Conference, 23-26 Jun 2003, Orlando, FL.Full text not available from this repository.
Figure of merit expressions for (a) fuel weight fraction in terms of range and aspect ratio and (b) propeller diameter in terms of power absorbed per blade have been derived. In the case of fuselage length heuristic approach has been adopted. Design and performance data of military propeller trainer airplanes, both piston props and turboprops, have been analyzed. Simple and effective correlations have been evolved for selecting fuel weight fraction, propeller diameter and fuselage length for baseline design configuration of military propeller trainer airplanes.
|Item Type:||Conference or Workshop Item (Paper)|
|Uncontrolled Keywords:||Propellant mass ratio;Figure of merit;Mass ratios;Propellers; Training aircraft;Military aircraft;Aspect ratio;Fuselages|
|Subjects:||AERONAUTICS > Aerodynamics|
|Depositing User:||M/S ICAST NAL|
|Date Deposited:||20 Nov 2006|
|Last Modified:||24 May 2010 09:53|
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