Aeronautics and astronautics: recent progress and future trends

R Martinez-Val, E Perez - Proceedings of the Institution of …, 2009 - journals.sagepub.com
Aeronautics and astronautics are two closely related disciplines, sometimes found under the
joint term aerospace, that have progressed at a formidable pace during the 20th century …

[HTML][HTML] Optimization of gas turbines for sustainable turbojet propulsion

YSH Najjar, IAI Balawneh - Propulsion and Power Research, 2015 - Elsevier
Gas-turbines are widely used to power aero planes because they are light, compact with a
high power-to-weight ratio. In the turbo jet engine, the main operating variables are …

[HTML][HTML] Adaptable conceptual aircraft design model

M Fioriti - Advances in aircraft and spacecraft science, 2014 - koreascience.kr
This paper presents a new conceptual design model ACAD (Adaptable Conceptual Aircraft
Design), which differs from the other models due to its considerable adaptability to the …

[PDF][PDF] Design Analysis and Modeling of a General Aviation Aircraft.

FH Darwish, GM Atmeh, ZF Hasan - Jordan Journal of Mechanical & …, 2012 - jjmie.hu.edu.jo
In the present study, design analysis is performed to accurately estimate the gross take-off
weight, define the external geometry, and size the wings and tail of a general aviation …

Lightweight design for an aircraft reinforcing frame based on structural bionics

D Xing, W Chen, D Xing, Z Li - Proceedings of the Institution …, 2013 - journals.sagepub.com
Lightweight design is urgently required in many fields, especially in aeronautics and
astronautics, but conventional design methods cannot always meet the requirement …

Design and analysis for development of a wing box static test rig

R Ramly, W Kuntjoro, W Wisnoe… - … Conference on Science …, 2010 - ieeexplore.ieee.org
Airplanes are designed to stay aloft with the help of wings on both sides. In operation at
cruising speed, the wings are subjected to load as much as the weight of the whole aircraft …

[PDF][PDF] Parametric Performance Analysis of a Mini Jet Engine

KK SHWE, Z AYE, T SWE - 2019 - ijsetr.com
Mini Jet Engines are widely used to power unmanned aeroplanes because they are light,
compact with a high powerto-weight ratio. In the mini jet engine, the main operating …

[PDF][PDF] DESIGN AND ANALYSIS OF THE INTERNAL WING AIRCRAFT (IWA) BY USING CFD

AD ALEXANDER, J JEEVAMALAR, K SUNDARAJAN - researchgate.net
ABSTRACT Computational Fluid Dynamics.: Unmanned Aerial Vehicles (UAVs) are
increasingly becoming the preferred medium for non-technical aerial missions. These …

[PDF][PDF] FINITE ELEMENT ANALYSIS OF STATIC WING BOX TEST RIG

AS Sathish, S SJ, VB Math - Citeseer
The design of airplane, when plane is in the flight mode it is because of wings on both sides.
While operating at the greater speed the wings are subjected to load which includes whole …

Improving the design of reinforcing frames by simulating the arch and peltate venation structures

X Deng-hai, C Wu-yi - Journal of Beijing Institute of Technology, 2014 - journal.bit.edu.cn
Based on the analyses on arch and peltate venation structures, the design of reinforcing
frames was improved. First, distribution rules of the arch structure were summarized …