Analogue/digital wind tunnel testing of active low momentum flow control on single and multi-component airfoil systems at high lift

2002 ◽  
Author(s):  
N. Lewington ◽  
D. Peake ◽  
F. Henry ◽  
C. Singh
Keyword(s):  
Wind Tunnel ◽  
Flow Control ◽  
Wind Tunnel Testing ◽  
High Lift ◽  
Tunnel Testing

Wind Tunnel Testing of Active Flow Control on the High Lift Common Research Model

2019 ◽  
Author(s):  
John C. Lin ◽  
LaTunia G. Pack Melton ◽  
Judith Hannon ◽  
Marlyn Andino ◽  
Mehti Koklu ◽  
...  
Keyword(s):  
Wind Tunnel ◽  
Flow Control ◽  
Active Flow Control ◽  
Wind Tunnel Testing ◽  
Research Model ◽  
High Lift ◽  
Active Flow ◽  
Tunnel Testing

scholarly journals High Lift Common Research Model for Wind Tunnel Testing: An Active Flow Control Perspective

2017 ◽  
Author(s):  
John C. Lin ◽  
LaTunia G. Pack Melton ◽  
Sally Viken ◽  
Marlyn Y. Andino ◽  
Mehti Koklu ◽  
...  
Keyword(s):  
Wind Tunnel ◽  
Flow Control ◽  
Active Flow Control ◽  
Wind Tunnel Testing ◽  
Research Model ◽  
High Lift ◽  
Active Flow ◽  
Tunnel Testing

Characterisation of a highly staggered spanwise cambered biplane

2015 ◽  
Vol 119 (1212) ◽  
pp. 203-228
Author(s):  
L.W. Traub ◽  
R. Waghela ◽  
K.A. Bordignon
Keyword(s):  
Numerical Simulation ◽  
Wind Tunnel ◽  
Dihedral Angles ◽  
Wind Tunnel Testing ◽  
High Lift ◽  
Front Wing ◽  
Geometric Variation ◽  
Tunnel Testing

AbstractAn investigation is presented to elucidate the performance of a staggered, spanwise cambered biplane. The spanwise camber yielded wings forming a ‘∧’ or ‘∨’ when viewed streamwise. The configuration is examined in terms of its aerodynamic and stability characteristics. The feasibility of negating the requirement for a conventional empennage is explored. Geometric variation encompassed front and back wing anhedral/dihedral angles yielding 49 combinations. Evaluation of the geometry was accomplished using both wind tunnel testing and numerical simulation. The results indicated that front wing dihedral in conjunction with aft wing anhedral was most beneficial, such that the benefit of wake spacing was maximised. Aerodynamic benefit was indicated compared to a conventional empennage geometry. The greatest disparity in behaviour of the fore and aft wing anhedral/dihedral distribution was in the high lift regime, where the nature of the stall varied. Simulations to establish the viability of the geometry in terms of controllability were also conducted and indicated that the configuration is viable.

Investigation and Improvement of High-Lift Aerodynamic Performances in Lowspeed Wind Tunnel Testing

2008 ◽  
Author(s):  
Yuzuru Yokokawa ◽  
Mitsuhiro Murayama ◽  
Masahiro Kanazaki ◽  
Katsuichi Murota ◽  
Takeshi Ito ◽  
...  
Keyword(s):  
Wind Tunnel ◽  
Wind Tunnel Testing ◽  
High Lift ◽  
Aerodynamic Performances ◽  
Tunnel Testing

scholarly journals Wind Tunnel Testing of Passive High-Lift Systems

2012 ◽  
Vol 4 (1) ◽  
pp. 67-75 ◽  
Author(s):  
PRICOP Mihai Victor ◽  
◽  
STOICA Corneliu ◽  
NAE Catalin ◽  
MUNTEANU Florin ◽  
...  
Keyword(s):  
Wind Tunnel ◽  
Wind Tunnel Testing ◽  
High Lift ◽  
Tunnel Testing

Wind Tunnel Testing of High Efficiency Low Power (HELP) Actuation for Active Flow Control

2020 ◽  
Author(s):  
John C. Lin ◽  
LaTunia G. Pack Melton ◽  
Judith Hannon ◽  
Marlyn Y. Andino ◽  
Mehti Koklu ◽  
...  
Keyword(s):  
Wind Tunnel ◽  
Low Power ◽  
Flow Control ◽  
High Efficiency ◽  
Active Flow Control ◽  
Wind Tunnel Testing ◽  
Active Flow ◽  
Tunnel Testing

Incremental wind tunnel testing of high lift systems

2016 ◽  
Author(s):  
Pricop Mihai Victor ◽  
Boscoianu Mircea ◽  
Crunteanu Daniel-Eugeniu
Keyword(s):  
Wind Tunnel ◽  
Wind Tunnel Testing ◽  
High Lift ◽  
Tunnel Testing
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