scholarly journals Fixed Boundary transition effect on transport aircraft aerodynamic characteristics under different Reynolds numbers

2021 ◽  
Vol 1985 (1) ◽  
pp. 012029
Author(s):  
Yuanjing Wang ◽  
Binbin Lv ◽  
Dawei Liu
Keyword(s):  
Reynolds Numbers ◽  
Aerodynamic Characteristics ◽  
Transition Effect ◽  
Fixed Boundary ◽  
Transport Aircraft

INVESTIGATION OF THE EFFECT OF ELASTIC DEFORMATIONS OF THE WING MODEL OF A WIDE-BODY COMMERCIAL TRANSPORT AIRCRAFT ON ITS AERODYNAMIC CHARACTERISTICS

2018 ◽  
Vol 49 (7) ◽  
pp. 771-780
Author(s):  
Valery Viktorovich Vozhdaev ◽  
Leonid Leonidovich Teperin
Keyword(s):  
Aerodynamic Characteristics ◽  
Elastic Deformations ◽  
Transport Aircraft ◽  
Wing Model

Influence of Upper Configuration on Aerodynamic Characteristics over Ishii Airfoil at Low Reynolds Numbers

2015 ◽  
Vol 63 (5) ◽  
pp. 217-224
Author(s):  
Kakeru YOSHIDA ◽  
Masafumi KAWABE ◽  
Kitai LEE ◽  
Asei TEZUKA
Keyword(s):  
Reynolds Numbers ◽  
Aerodynamic Characteristics ◽  
Low Reynolds Numbers ◽  
Low Reynolds

scholarly journals Features of flow around transport aircraft model with running propellers by modelled engine failure in wind tunnel

2021 ◽  
Vol 2103 (1) ◽  
pp. 012206
Author(s):  
V I Chernousov ◽  
A A Krutov ◽  
E A Pigusov
Keyword(s):  
Wind Tunnel ◽  
Lift Coefficient ◽  
Aerodynamic Characteristics ◽  
Light Transport ◽  
Transport Aircraft ◽  
Engine Failure ◽  
The One ◽  
Low Speed Wind Tunnel ◽  
Control Surfaces ◽  
Landing Mode

Abstract This paper presents the experiment results of modelling the one engine failure at the landing mode on a model of a light transport airplane in the T-102 TsAGI low speed wind tunnel. The effect of starboard and port engines failure on the aerodynamic characteristics and stability of the model is researched. The model maximum lift coefficient is reduced about ≈8% and there are the same moments in roll and yaw for starboard and port engines failure case. It was found that the failure of any engine has little impact on the efficiency of control surfaces. Approaches of compensation of forces and moments arising in the engine failure case were investigated.

scholarly journals CFD Analysis of Aerodynamic Characteristics of a BWB UCAV configuration with Transition effect

2014 ◽  
Vol 42 (7) ◽  
pp. 535-543
Author(s):  
Young-Hee Jo ◽  
Kyoungsik Chang ◽  
Dong-Jin Sheen ◽  
Soo Hyung Park
Keyword(s):  
Aerodynamic Characteristics ◽  
Cfd Analysis ◽  
Transition Effect

Aerodynamic Characteristics of Elliptic Airfoils in High Reynolds Numbers

2008 ◽  
Vol 45 (2) ◽  
pp. 641-650 ◽  
Author(s):  
Sungyoon Choi ◽  
Oh Joon Kwon
Keyword(s):  
Reynolds Numbers ◽  
Aerodynamic Characteristics ◽  
High Reynolds Numbers ◽  
High Reynolds
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