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Conceptual Design Code Validation and Optimization of Aircraft for Minimum Drag and Maximum Range

Volume: 20  ,  Issue: 1 , January    Published Date: 22 January 2019
Publisher Name: IJRP
Views: 882  ,  Download: 519

Authors

# Author Name
1 Banyar Thein

Abstract

This paper develops conceptual design code and validate with existing results of Single Seat Aerobatic aircraft (SSA) by the user requirements.  Special consideration is given to minimize total Drag, maximum Range for optimum conceptual design based on developed design code.

Keywords

  • Conceptual Design; Validation; Range; Total Drag