scholarly journals CFD analysis of the aerodynamic characteristics of biconvex airfoil at compressible and high Mach numbers flow

2019 ◽  
Vol 1 (10) ◽  
Author(s):  
Ebrahim Hosseini
AIAA Journal ◽  
1970 ◽  
Vol 8 (2) ◽  
pp. 294-300 ◽  
Author(s):  
C. J. WELSH ◽  
G. L. WINCHENBACH ◽  
A. N. MADAGAN

2021 ◽  
Vol 2089 (1) ◽  
pp. 012024
Author(s):  
S Kale ◽  
E Pendharkar

Abstract Blended Wing Body is a revolutionary concept offering phenomenal performance advantages over conventional aircraft. There are various aerodynamic features that are added to the wing in order to adjust the lift distribution and wing twist is one of them. This paper presents a progressive study to examine the effects of twist angles on the aerodynamic characteristics of a Blended Wing Body (BWB) aircraft. CFD analysis is carried out on seven BWB models having wing twists ranging from +3° to -3°. Each model is analyzed at four different Mach numbers. The coefficient of drag (Cd) and coefficient of lift (Cl) is determined and plotted against the twist angle to obtain a trend. The Cl/Cd ratio is also calculated to observe the overall aerodynamic performance of the BWB.


An experimental study has been made of the gaseous drag torque on an isolated sphere rotating at high Mach numbers. The sphere was suspended electromagnetically and spun by induction. The drag torque has been measured through the transition régime from continuum to free molecule flow at Mach numbers (based on equatorial speed) of up to about five. These high Mach numbers were achieved in heavy vapours (diiodomethane, germanium tetrabromide and stannic bromide) with sonic speed as little as a quarter of that in air. To measure the pressure in the vapour a second (smaller) rotating sphere was used as a pressure gauge. The results agree well with those previously obtained and show an unexpected Mach number dependence in the transition régime.


1968 ◽  
Vol 13 (2) ◽  
pp. 56-64
Author(s):  
W. H. Tanner ◽  
J. F. VanWyckhouse ◽  
Patrick Cancro ◽  
John McCloud

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