Linear correlations of principal parameters for the preliminary design of twin civil jet aircraft
Identifieur interne : 000134 ( Main/Exploration ); précédent : 000133; suivant : 000135Linear correlations of principal parameters for the preliminary design of twin civil jet aircraft
Auteurs : Yannis Kallinderis [Grèce] ; Xenakis Vouvakos [Grèce] ; Pinelopi Menounou [Grèce]Source :
- Aircraft Engineering and Aerospace Technology [ 0002-2667 ] ; 2009-10-16.
English descriptors
- Teeft :
- Aeronautical engineering, Aerospace technology, Aiaa paper, Aircraft aircraft engineering, Aircraft design, Aircraft design parameters, Aircraft height, Aircraft noise, Approach speed, Baggage weight, Baseline design, Btail, Correlated parameters, Correlated quantities, Correlation equations, Database, Design parameters, Design process, Elevator area, Empty weight, Engine parameters, Engine thrust, Epndb, Epnl, Epnl values, Federal aviation regulations, Figures show, Flaps area, Fuel weight, Fuselage, Fuselage length, Good correlation, Gross weight, Horizontal tail span, Initial estimate, Initial evaluation, International journal yannis kallinderis, International standards, Kallinderis, Landing weight, Linear correlations, Linear relationships, Maximum aircraft weight, Maximum altitude, Maximum weight, Menounou, Nasa history, Noise amplitude, Noise amplitudes, Noise data, Noise level, Noise levels, Noise measurements, Overall height, Parameter, Payload, Payload weight, Pinelopi, Pinelopi menounou volume, Plot method, Preliminary design, Preliminary design parameters, Preliminary design process, Present work, Principal parameters, Rudder, Rudder area, Selev, Several books, Sideline, Sideline epnl correlates, Sideline noise, Simple correlations, Smaller aircraft, Srud, Strong correlations, Tail section, Tailplane span, Vouvakos, Wing area, Wing chord, Wing chords, Wing span, Xenakis, Xenakis vouvakos, Yannis.
Abstract
Purpose The purpose of this paper is to simplify the preliminary design process as well as the initial evaluation of existing design parameters of civil jet aircraft to include noise level consideration right from the start of the design process and to form a current database of civil jet aircraft design parameters. Designmethodologyapproach Simple linear correlations are found between key design parameters. Findings Direct linear relationships are found between design parameters including noise levels. Simplified preliminary design process. Originalityvalue New correlations which simplify the current procedures for preliminary design. In addition, the noise is included right from the beginning of the design. Finally, a new database is formed with specially selected aircraft that is current and covers a wide spectrum of sizes.
Url:
DOI: 10.1108/00022660910997801
Affiliations:
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<term>Aircraft design</term>
<term>Aircraft design parameters</term>
<term>Aircraft height</term>
<term>Aircraft noise</term>
<term>Approach speed</term>
<term>Baggage weight</term>
<term>Baseline design</term>
<term>Btail</term>
<term>Correlated parameters</term>
<term>Correlated quantities</term>
<term>Correlation equations</term>
<term>Database</term>
<term>Design parameters</term>
<term>Design process</term>
<term>Elevator area</term>
<term>Empty weight</term>
<term>Engine parameters</term>
<term>Engine thrust</term>
<term>Epndb</term>
<term>Epnl</term>
<term>Epnl values</term>
<term>Federal aviation regulations</term>
<term>Figures show</term>
<term>Flaps area</term>
<term>Fuel weight</term>
<term>Fuselage</term>
<term>Fuselage length</term>
<term>Good correlation</term>
<term>Gross weight</term>
<term>Horizontal tail span</term>
<term>Initial estimate</term>
<term>Initial evaluation</term>
<term>International journal yannis kallinderis</term>
<term>International standards</term>
<term>Kallinderis</term>
<term>Landing weight</term>
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<term>Linear relationships</term>
<term>Maximum aircraft weight</term>
<term>Maximum altitude</term>
<term>Maximum weight</term>
<term>Menounou</term>
<term>Nasa history</term>
<term>Noise amplitude</term>
<term>Noise amplitudes</term>
<term>Noise data</term>
<term>Noise level</term>
<term>Noise levels</term>
<term>Noise measurements</term>
<term>Overall height</term>
<term>Parameter</term>
<term>Payload</term>
<term>Payload weight</term>
<term>Pinelopi</term>
<term>Pinelopi menounou volume</term>
<term>Plot method</term>
<term>Preliminary design</term>
<term>Preliminary design parameters</term>
<term>Preliminary design process</term>
<term>Present work</term>
<term>Principal parameters</term>
<term>Rudder</term>
<term>Rudder area</term>
<term>Selev</term>
<term>Several books</term>
<term>Sideline</term>
<term>Sideline epnl correlates</term>
<term>Sideline noise</term>
<term>Simple correlations</term>
<term>Smaller aircraft</term>
<term>Srud</term>
<term>Strong correlations</term>
<term>Tail section</term>
<term>Tailplane span</term>
<term>Vouvakos</term>
<term>Wing area</term>
<term>Wing chord</term>
<term>Wing chords</term>
<term>Wing span</term>
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<front><div type="abstract">Purpose The purpose of this paper is to simplify the preliminary design process as well as the initial evaluation of existing design parameters of civil jet aircraft to include noise level consideration right from the start of the design process and to form a current database of civil jet aircraft design parameters. Designmethodologyapproach Simple linear correlations are found between key design parameters. Findings Direct linear relationships are found between design parameters including noise levels. Simplified preliminary design process. Originalityvalue New correlations which simplify the current procedures for preliminary design. In addition, the noise is included right from the beginning of the design. Finally, a new database is formed with specially selected aircraft that is current and covers a wide spectrum of sizes.</div>
</front>
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