The preliminary design of the air-intake system and the nacelle in the small aircraft-engine integration process

Author： Stalewski Wienczyslaw   Zóltak Jerzy  

Publisher： Emerald Group Publishing Ltd

ISSN： 0002-2667

Source： Aircraft Engineering, Vol.86, Iss.3, 2014-04, pp. : 250-258

Disclaimer: Any content in publications that violate the sovereignty, the constitution or regulations of the PRC is not accepted or approved by CNPIEC.

Previous Menu Next

Related content

The Design of the Test Control System of Small Piston Aircraft Engine

By  

Advanced Materials Research, Vol. 2014, Iss. 1061, 2015-01 ,pp. : 912-915

Trans Tech Publications

Access to resources Recommend Favorite

Optimized bio-inspired stiffening design for an engine nacelle

By Lazo Neil   Vodenitcharova Tania   Hoffman Mark  

Bioinspiration & Biomimetics, Vol. 10, Iss. 6, 2015-12 ,pp. : 66008-66021

IOP Publishing

Access to resources Recommend Favorite

Multi-Objective Climb Path Optimization for Aircraft/Engine Integration Using Particle Swarm Optimization

By Antonakis Aristeidis   Nikolaidis Theoklis   Pilidis Pericles  

Applied Sciences, Vol. 7, Iss. 5, 2017-04 ,pp. : 469-469

MDPI

Access to resources Recommend Favorite

Aerodynamic design and experimental modelling of an innovative supersonic three-dimensional air-intake

By  

The Aeronautical Journal, Vol. 117, Iss. 1192, 2013-06 ,pp. : 559-584

Cambridge University Press

Access to resources Recommend Favorite

Piston Engine Intake and Exhaust System Design

By Davies P.O.A.L.  

Journal of Sound and Vibration, Vol. 190, Iss. 4, 1996-03 ,pp. : 677-712

Academic Press

Access to resources Recommend Favorite