Experimental Investigation of Aerodynamic Characteristics on Slender Bodies at High Angles of Attack

2003 ◽  
Vol 49 (1) ◽  
pp. 31-40 ◽  
Author(s):  
Peiqing Liu ◽  
Xueying Deng
Keyword(s):  
Experimental Investigation ◽  
Aerodynamic Characteristics ◽  
Slender Bodies ◽  
High Angles Of Attack

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

SINGULAR AERODYNAMIC FEATURES OF LOW-SPEED HIGH-ANGLES-OF-ATTACK SLENDER BODIES

1988 ◽  
pp. 435-440
Author(s):  
K. Suzuki ◽  
M. Matsuzaka ◽  
T. Watanuki ◽  
N. Itoda ◽  
H. Kubota
Keyword(s):  
Low Speed ◽  
Slender Bodies ◽  
High Angles Of Attack

An experimental investigation on the aerodynamic characteristics of NACA 4412 with winglets

2019 ◽  
Author(s):  
Ismat Ara ◽  
Mohammad Ali ◽  
Md. Quamrul Islam ◽  
Most. Nasrin Akhter
Keyword(s):  
Experimental Investigation ◽  
Aerodynamic Characteristics

Aerodynamic characteristics of the MMPT ATD vehicle at high angles of attack

1993 ◽  
Author(s):  
EDMUND SMITH ◽  
MICHAEL SALAZAR ◽  
S. HEBBAR ◽  
M. PLATZER
Keyword(s):  
Aerodynamic Characteristics ◽  
High Angles Of Attack

Aerodynamic characteristics of delta wing–body combinations at high angles of attack

1994 ◽  
Vol 98 (975) ◽  
pp. 159-170 ◽  
Author(s):  
P. R. Viswanath ◽  
S. R. Patil
Keyword(s):  
Vortex Breakdown ◽  
Delta Wing ◽  
Aerodynamic Characteristics ◽  
Surface Flow ◽  
Flow Visualisation ◽  
Symmetric Flow ◽  
Gradual Process ◽  
Wing Sweep ◽  
The Mean ◽  
High Angles Of Attack

AbstractAn experimental study investigating the aerodynamic characteristics of generic delta wing-body combinations up to high angles of attack was carried out at a subsonic Mach number. Three delta wings having sharp leading edges and sweep angles of 50°, 60° and 70° were tested with two forebody configurations providing a variation of the nose fineness ratio. Measurements made included six-component forces and moments, limited static pressures on the wing lee-side and surface flow visualisation studies. The results showed symmetric flow features up to an incidence of about 25°, beyond which significant asymmetry was evident due to wing vortex breakdown, forebody vortex asymmetry or both. At higher incidence, varying degrees of forebody-wing vortex interaction effects were seen in the mean loads, which depended on the wing sweep and the nose fineness ratio. The vortex breakdown on these wings was found to be a gradual process, as implied by the wing pressures and the mean aerodynamic loads. Effects of forebody vortex asymmetry on the wing-body aerodynamics have also been assessed. Comparison of Datcom estimates with experimental data of longitudinal aerodynamic characteristics on all three wing-body combinations indicated good agreement in the symmetric flow regime.

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