Engineering & Technology

Engineering & Technology

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

Pages: 8  ,  Volume: 20  ,  Issue: 1 , January   2019
Received: 16 Jan 2019  ,  Published: 22 January 2019
Views: 113  ,  Download: 54

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
  • References

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