Conceptual Design Code Validation and Optimization of Aircraft for Minimum Drag and Maximum Range
Authors:Banyar Thein
Open Access
Journal Type:Research Article
Subject Field:Applied Engineering
Downloads:844
Publish Date:January 21, 2019 7:00 pm
Views:1264
Volume:20, Issue: 1, January, 2019
Subject:Engineering & Technology
Pages:null-null
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.