Drag reduction analysis of wing airfoil E562 with forward wingtip fence at cant angle variations of 75° and 90°

S Sutardi, WA Widodo - AIP conference proceedings, 2018 - pubs.aip.org
Airfoil modeling is very important especially in determining the airfoil's performance. One
very important in the airfoil design is how to make airfoil with high lift and low drag to obtain …

Numerical study of flow characteristics around wing airfoil Eppler 562 with variations of rearward wingtip fence

SP Setyo Hariyadi, S Sutardi… - AIP Conference …, 2018 - pubs.aip.org
To produce lift on the wing of the aircraft, pressure distribution on the upper surface of the
wing must be lower than the pressure on the lower of the wing. This can be done by making …

[PDF][PDF] Studi numeric karakteristik aliran tiga dimensi di sekitar airfoil eppler 562 dengan penambahan forward wingtip fence variasi cant angle 90⁰, 85⁰, 80⁰

AS Panjaitan - 2017 - repository.its.ac.id
Winglet sebagai bentuk usaha mengurangi timbulnya wingtip vortex telah berkembang
cukup pesat didunia penerbangan. Berbagai macam jenis winglet telah dikembangkan …

Computational Study on Induced Drag Reduction of Electric Aircraft Wing Using Various Winglet Configurations

S Malathi, TR Kamalakrishna, D Ramakrishna… - International Conference …, 2023 - Springer
The addition of winglets provides an increased aerodynamic efficiency without any other
drastic changes to the structure of the aircraft. Although many modern airliners are equipped …

STUDI EKSPERIMEN TUFT FLOW VISUALIZATION PADA FORWARD WINGTIP FENCE CANT ANGLE 75o TERHADAP KINERJA AERODINAMIKA WING AIRFOIL …

S Hariyadi, M Sagala - Approach: Jurnal Teknologi …, 2020 - repo.poltekbangsby.ac.id
Winglet adalah salah satu aksesoris pada sayap pesawat yang memungkinkan
penambahan performansi sayap tanpa harus memperpanjang wingspan (bentangan sayap …

Generation and Analysis of Streamwise Vortices from Vortex Tube Apparatus

BMK Carlson - 2020 - search.proquest.com
A pressurized vortex tube is used to generate streamwise vortices in a wind tunnel and the
resulting flow behavior is analyzed. The apparatus is intended to verify computational data …

Experimental and Computational Analysis of Bio-Inspired Winglets for Micro Air Vehicles

A Sathyabhama, AM Rajiv, I Sai Sandeep… - Journal of Applied …, 2021 - jafmonline.net
Micro Air Vehicles (MAVs) are increasingly being used for civil and military surveillance. As
the surveillance requirements are increasing, improving the range of MAVs becomes …

Comparative Study of Forward Wingtip Fence and Rearward Wingtip Fence on Wing Airfoil Eppler E562

S Hariyadi, S Sutardi, WA Widodo… - Journal of Energy …, 2020 - ejournal.umm.ac.id
The perfect wing is a dream that many airplanes has manufactured have been striving to
achieve since the beginning of the airplane design. There are some aspect that most …

[PDF][PDF] COMPUTATIONAL STUDY ON FLOW CHARACTERISTICS OF A TAPERED WING WITH MODIFIED RAKED WINGTIP FOR REGIONAL AIRCRAFT

MS Prasath, G Sivaraj, D Lakshmanan… - Indian Journal of …, 2021 - ijest.bitsathy.ac.in
A wingtip is an essential part of an aircrafts located the tip of the wing of an aircraft. It helps to
reduce the vortices created at the tip of the wings. Thereby reducing the drag produces and …

STUDI EKSPERIMEN TUFT FLOW VISUALIZATION PADA FORWARD WINGTIP FENCE CANT ANGLE 75o TERHADAP KINERJA AERODINAMIKA WING

M Sagala, S Hariyadi - Approach: Jurnal Teknologi …, 2020 - ejournal.poltekbangsby.ac.id
Winglet is one of the accessories on the aircraft's wing that allows the addition of wing
performance without having to widen the wingspan (stretch of the wing). Winglets can be in …