Aerodynamic Characteristics of Hypersonic Vehicle with Variable Sweep back Wing Configuration

2009 ◽  
Vol 5 (1) ◽  
pp. 44-50
Author(s):  
P. Saravanan ◽  
◽  
S. Nadaraja Pillai ◽  
K.M. Parammasivam ◽  
◽  
...  
Keyword(s):  
Aerodynamic Characteristics ◽  
Hypersonic Vehicle

Numerical Study on Aerodynamic Design of Hypersonic Vehicle Forebody

2013 ◽  
Vol 756-759 ◽  
pp. 4626-4629
Author(s):  
Fang Wang ◽  
Shuang Lin Gao
Keyword(s):  
Mach Number ◽  
Numerical Study ◽  
Wedge Angle ◽  
Lower Surface ◽  
Aerodynamic Characteristics ◽  
Hypersonic Vehicle ◽  
Lateral Flow ◽  
Aerodynamic Design ◽  
High Efficient ◽  
Angle Method

The lift forebody configuration of a small hypersonic vehicle is designed by using the wedge angle method in this paper. The lift forebody created has been optimized by the simplex method with a penalty function. The aerodynamic characteristics of the forebody optimized are investigated by numerical method. The research results show that the wedge angle method is a high efficient way to generate the lift forebody of the hypersonic vehicle; On the design mach number, there is pressure leaking between the upper and lower surface of lift forebody, which leads to lateral flow in the spanwise on the precompression plane, and which create the unhomogeneity of inlet flow field; Adding side skirts on the both sides, which can reduce the lateral flow on the forebody's precompression plane, it can raise the forebody lift.

NUMERICAL AND EXPERIMENTAL INVESTIGATION OF AERODYNAMIC CHARACTERISTICS OF THE HYPERSONIC AIRCRAFT MODEL OF INTEGRATED CONFIGURATION

2013 ◽  
Vol 44 (1) ◽  
pp. 111-127
Author(s):  
Sergey Mikhailovich Zadonsky ◽  
Alexander Petrovich Kosykh ◽  
Garry Grantovich Nersesov ◽  
Iraida Fedorovna Chelysheva ◽  
Sergey Valer'evich Chernov ◽  
...  
Keyword(s):  
Experimental Investigation ◽  
Aerodynamic Characteristics ◽  
Aircraft Model ◽  
Hypersonic Aircraft

INFLUENCE OF HIGH-BYPASS-RATIO TURBOFAN JETS ON AERODYNAMIC CHARACTERISTICS OF HIGH-LIFT WING

2015 ◽  
Vol 46 (7) ◽  
pp. 619-629
Author(s):  
Albert Vasilievich Petrov ◽  
Vladimir Fedorovich Tretyakov
Keyword(s):  
Aerodynamic Characteristics ◽  
High Lift ◽  
Bypass Ratio

Aerodynamic Characteristics of Conical Nose with Axisymmetric Cavities

2007 ◽  
Vol 55 (641) ◽  
pp. 304-308
Author(s):  
Yusuke Maru ◽  
Hiroaki Kobayashi ◽  
Motoyuki Hongoh ◽  
Tetsuya Sato
Keyword(s):  
Aerodynamic Characteristics ◽  
Axisymmetric Cavities

Aerodynamic characteristics of a large-scale, twin tilt-nacelle V/STOL model

1981 ◽  
Author(s):  
M. FALARSKI ◽  
M. DUDLEY ◽  
W. BUCHMANN ◽  
A. PISANO
Keyword(s):  
Large Scale ◽  
Aerodynamic Characteristics
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