[HTML][HTML] A computational method to study heat transfer in a helicopter turboshaft engine compartment for waste energy recovery purposes

P Fernández-Yáñez, AJ Fernández-López… - Applied Thermal …, 2024 - Elsevier
It is important to take action to make aviation more energy-efficient and less pollutant. One of
the approaches currently under development is waste energy recovery. This would be …

Challenges of turboprop engine installation on small aircraft

P Guła, D Ulma, K Żurek, R Żurawski - Aircraft Engineering and …, 2019 - emerald.com
Purpose The purpose of this paper is to present the challenges of turbine engine installation
on small aircraft. The work was a part of the European Union project Efficient Systems and …

Investigation of a cooling system for a hybrid airplane

R Kabir, K Kaddoura, FP McCluskey… - 2018 AIAA/IEEE …, 2018 - ieeexplore.ieee.org
Airplane cooling process can be performed with the help of two different techniques. One is
global cooling system and the other is local cooling system. The goal of present paper is to …

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

W Stalewski, J Żółtak - Aircraft Engineering and Aerospace …, 2014 - emerald.com
Purpose–The purpose of this paper is to present the results of the preliminary design and
optimization of the air-intake system and the engine nacelle. The work was conducted as …

Comparison of 1D and 3D thermal models of the nacelle ventilation system in a small airplane

P Łapka, M Bakker, P Furmański… - Aircraft Engineering and …, 2018 - emerald.com
Purpose Insight in the temperature distribution on the internal and external surface of the
nacelle is of great importance during the design phase of an aircraft. However, detailed …

CFD simulation of engine nacelle cooling on pusher configuration aircraft

A Olejnik, A Dziubiński, Ł Kiszkowiak - Aircraft Engineering and …, 2021 - emerald.com
Purpose The purpose of this paper is to simulate with in-depth reconstruction of existing
geometry a process of cooling of the aircraft engine in pusher configuration, which is more …

Investigation of thermal interactions between the exhaust jet and airplane skin in small aircrafts

P Łapka, M Seredyński… - … in Computational Fluid …, 2019 - inderscienceonline.com
An advanced numerical model of the exhaust jet and its thermal interaction with the aircraft
body (fuselage, wings and flaps) was developed in this paper and then applied for …

Analysis of cooling of the exhaust system in a small airplane by applying the ejector effect

Ł Złoty, P Łapka, P Furmański - Journal of Power Technologies, 2018 - papers.itc.pw.edu.pl
This paper presents a thermal analysis of elements of the exhaust system of the redesigned
airplane I-23. In order to improvethe thermal performance of the exhaust system and …

Investigation of thermal interactions between elements of propulsion system and selected parts of the airplane skin in small aircrafts

P Łapka, M Seredyński… - Archives of …, 2018 - yadda.icm.edu.pl
Abstract Development of new or upgrading of existing airplanes requires many different
analyses, eg, thermal, aerodynamical, structural, and safety. Similar studies were performed …

CFD Assessment of an Ultralight Aircraft Including In-Flight Test Data Comparison

G Zipszer, B Darázs, A Horváth, D Toma… - … -European Journal of …, 2023 - journals.ub.ovgu.de
CFD Assessment of an Ultralight Aircraft Including In-Flight Test Data Comparison Page 1
TECHNISCHE MECHANIK an open access journal journal homepage: www.ovgu.de/techmech …