Comparison of Aerodynamics Characteristics of NACA 0015 & NACA 4415

RI Rubel, MK Uddin, MZ Islam, M Rokunuzzaman - 2016 - preprints.org
NACA 0015 and NACA 4415 aerofoil are most common four digits and broadly used
aerodynamic shape. Both of the shapes are extensively used for various kind of applications …

Acquisition of signals in a wind tunnel using the dasylab software package

K Pytel, Z Szczerba, I Farmaha… - 2020 IEEE XVIth …, 2020 - ieeexplore.ieee.org
This publication presents the use of the acquisition of signals in a wind tunnel using the
DasyLab system to assess the suitability of selected airfoils for the power industry and is a …

[PDF][PDF] Comparative Flow Analysis of NACA S6061 and NACA 4415 Aerofoil by Computational Fluid Dynamics

S Roy - International Journal of Mechanical Engineering (IJME) … - academia.edu
In this study, a comparison has been drawn between the flow analysis of NACA S6061 and
NACA 4415 aerofoil. The application of both airfoils is different. Here at zero angle of attack …

[PDF][PDF] Effect of Angle of Attack on Lift, Drag, Pitching Moment and Pressure Distribution of NACA 4415 Wing

NA Ismail, MU Kaisan, MB Balogun… - Journal of science …, 2020 - researchgate.net
This experiment was conducted to determine the effects of angle of attack on lift, drag,
pitching moment and pressure distribution during the flow of NACA 4415 wing model of …

Numerical studies on aerodynamic performance of NACA 0018 profile in fundamental and research application of the aerospace industry

EI Apostol, AM Ţîţu - Journal of Physics: Conference Series, 2023 - iopscience.iop.org
For a good functioning of the activities carried out within research institutions both at
managerial level and for fulfilling the technical requirements, we aim to determine the …

[PDF][PDF] Analisis Airfoil Double-Slot Flap LS (01)-0417 MOD Dengan Airfoil Tanpa Flap Nasa SC (2) 0610

G Jatisukamto, M Sari - Jurnal Energi Dan Manufaktur, 2018 - academia.edu
Kestabilan pesawat terbang ditentukan oleh desain airfoil sayap dan ekor. Perbedaan
kecepatan aliran udara antara permukaan atas dan bawah airfoil menghasilkan perbedaan …

Desain FW UAV Model Pylon dan Fighter Untuk Kecepatan Manuver Lintasan Angka 8

N Hanafi, N Tamami, AS Herwanda… - Journal of Electrical …, 2023 - ejournal.unuja.ac.id
Salah satu kemampuan dasar wahana terbang type fixedwing adalah dapat lepas landas
pada area yang terbatas, terbang cepat mencapai lokasi yang diinginkan secara aman …