Robust Design of High Speed Natural-Laminar-Flow Airfoil for High Lift

2017 ◽  
Author(s):  
Huan Zhao ◽  
Zhenghong Gao ◽  
Chao Wang ◽  
Gao Yuan
Keyword(s):  
Laminar Flow ◽  
Robust Design ◽  
High Speed ◽  
High Lift ◽  
Natural Laminar Flow

High-Lift Simulations of Slotted, Natural-Laminar-Flow Airfoils with Drooped Leading Edge

2020 ◽  
Author(s):  
Hector D. Ortiz-Melendez ◽  
Ethan Long ◽  
George Toth ◽  
Kathryn Keely ◽  
James G. Coder
Keyword(s):  
Laminar Flow ◽  
Leading Edge ◽  
High Lift ◽  
Natural Laminar Flow

scholarly journals High Lift Configuration of a Slotted Natural Laminar Flow Airfoil

2019 ◽  
Author(s):  
Dan Twiss ◽  
Christopher Colletti ◽  
Phillip J. Ansell
Keyword(s):  
Laminar Flow ◽  
High Lift ◽  
Natural Laminar Flow

Robust Design of a Supersonic Natural Laminar Flow Wing-Body

2017 ◽  
Vol 12 (4) ◽  
pp. 14-27 ◽  
Author(s):  
Domenico Quagliarella ◽  
Emiliano Iuliano
Keyword(s):  
Laminar Flow ◽  
Robust Design ◽  
Natural Laminar Flow

High-Lift Simulations of Slotted, Natural-Laminar-Flow Airfoils

2019 ◽  
Author(s):  
Hector D. Ortiz-Melendez ◽  
James G. Coder ◽  
Arvin Shmilovich
Keyword(s):  
Laminar Flow ◽  
High Lift ◽  
Natural Laminar Flow

High-Lift Computational Strategy for Slotted, Natural-Laminar-Flow Airfoils

2021 ◽  
pp. 1-15
Author(s):  
Hector D. Ortiz-Melendez ◽  
James G. Coder ◽  
Arvin Shmilovich
Keyword(s):  
Laminar Flow ◽  
High Lift ◽  
Natural Laminar Flow ◽  
Computational Strategy

The Development of Very Light Jet with Unconventional Arrangement

2011 ◽  
Vol 110-116 ◽  
pp. 2219-2227
Author(s):  
Siti Zawiah Md Dawal ◽  
Tuan Ya Tmys ◽  
Yusuf Khairi ◽  
Nukman Yusoff ◽  
Ahmad Yazid Aznijar
Keyword(s):  
High Speed ◽  
Operational Flexibility ◽  
High Lift ◽  
Current Trends ◽  
Surface Configuration ◽  
New Concepts ◽  
Aircraft Performance ◽  
Design Requirements ◽  
Natural Laminar Flow ◽  
Light Jet

In order to be economically viable and competitive, the current trends in designing very light jet aircraft have shown that it is essential to improve the aircraft performance and operational flexibility goal, nevertheless have an efficient cost. The application of unconventional configuration has attracted the designer to achieve that goal. This paper discusses the prospective design of unconventional arrangement which will be applied for very light jet aircraft. The existing of a very light jet configurations is reviewed. New concepts of unconventional configuration for this type of aircraft are discussed. The three-surface configuration is then proposed for the design project. The configuration offers stability and unobstructed cabin. With the appropriate design, the additional weight and interference drag due to the extra surface can be reduced. The new design of aircraft configuration and cabin are discussed. High Speed Natural Laminar Flow airfoil is applied to obtain High Lift/Drag Wing design. The weight and aircraft performances are then estimated. The predicted aircraft performance has satisfied the design requirements and objectives. The design process covered by this paper is only concentrate on initial design. The data from this paper can be continuing in future for the next step of design.

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