Preliminary Design Calculation for a Business Jet Aircraft
| Vol-2 | Issue-4 | April 2017 | Published Online: 10 April 2017 PDF ( 247 KB ) | ||
| Author(s) | ||
| Indhumathi E. 1; Rengasamy N.V. 2 | ||
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1Department of Aeronautical Engineering, RVS Educational Trust’s Group of Institutions, Dindigul, Tamil Nadu, (India) 2Department of Aeronautical Engineering, RVS Educational Trust’s Group of Institutions, Dindigul, Tamil Nadu, (India) |
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| Abstract | ||
The purpose of this paper is to calculate the preliminary design for a business jet aircraft in an existing formulas and procedures. The equations are obtained to form a Aircraft design methodology. This methodology is used to obtain the fundamental parameter for a business jet aircraft such as gross weight, thrust estimation, lift and drag calculations, power, and performance parameters. |
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