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Category Archives: Aircraft Design

Aerodinamic for compressible gas

Posted on May 16, 2015 by Aerospace Engineering

1 – Introduction 2 – Aerodinamic for compressible gas – Basic principles 3 – Performance of Jet Engine 4 – … Continue reading →

Posted in Turbofan | Tagged Aerodinamic, compressible, condition | Leave a comment

Verifying of a fuselage frame symmetrically loaded

Posted on October 21, 2014 by Aerospace Engineering

The fuselage frame is a principal structural element of the aircraft shell structure, it is important for the following reasons: … Continue reading →

Posted in Aircraft Design | Tagged analysis, compression, diagram, frame, Menabrea, mises, shear, skin, stringer, symmetrically, tension | Leave a comment

Preliminary sizing – Matching Chart

Posted on June 26, 2014 by Aerospace Engineering

Introduction This article introduces the first step in the preliminary sizing process, which is to determine the so-called aircraft … Continue reading →

Posted in Aircraft Design | Tagged Approach, chart, climb, Cruise, distance, drag, Landing, lift, Mach, matching, Missed, Power, Preliminary, sizing | Leave a comment

Winglets

Posted on July 28, 2013 by Aerospace Engineering

Wingtip devices are usually intended to improve the efficiency of fixed-wing aircraft. There are several types of wingtip devices, and although they function … Continue reading →

Posted in Wing | Tagged aerodynamic, aircraft, airflow, downstream, drag, edge, ellipse, Elliptical, induced, lift, spanwise, trailing, vortex, wing, WINGLET, WINGLETS, WINGLETS WINGLET wing aircraft, wingtip | Leave a comment

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