Comparative study of two dimensional boundary layer over
NACA 23012 and NACA 23021 airfoils by using keller’s box
method

QR Code

Comparative study of two dimensional boundary layer over NACA 23012 and NACA 23021 airfoils by using keller’s box method

This paper begins with general description on various methods for solving boundary layer equation. In particular, Prandtl's boundary layer equation is a simplified version of Navier-Stokes equation that is solved integrally. Order of magnitude analysis can be used to solve laminar and turbu...

Full description

Bibliographic Details
Main Authors:	Kumar, Vinod Kumar K Sivak, Abdullah, Aslam, Basuno, Bambang
Format:	Article
Language:	English
Published:	Penerbit UTHM 2022
Subjects:	T Technology (General)
Online Access:	http://eprints.uthm.edu.my/7709/ http://eprints.uthm.edu.my/7709/1/J14547_893fab78e8617407a58a635075219a9d.pdf

Similar Items

Vortex formation in unsteady flow over NACA 4412 and NACA 4424 airfoils
by: Hadi, Muhammad Irfan, et al.
Published: (2020)

Evolution of NACA23012 wake vortices structure using PIV
by: Elsayed, Omer Ali, et al.
Published: (2012)

Comparative study of turbulent incompressible flow past naca airfoils
by: Abdullah, Aslam, et al.
Published: (2018)

Aerodynamic Characteristics Of Membrane Airfoil Compared To Rigid Naca 4412 Airfoil
by: Chan, Min Xhao
Published: (2018)

Aerodynamics Study Of Tubercle Effect On NACA4412 Airfoil
by: Enso, Ennelyn Novema
Published: (2017)

Effect Of Vibration Frequency On Naca 4412 Airfoil Aerodynamic Performance
by: Chan, Ze Yu
Published: (2019)

Discrete tonal noise of NACA0015 airfoil at low reynolds number
by: Andan, Amelda Dianne, et al.
Published: (2019)

Creating and simulating turbulence generation on NACA S1046 airfoil with CFD software
by: Erwin, Erwin, et al.
Published: (2024)

Drag Reduction On Naca 2412 Using Dimpled Airfoil And Grooved Wing
by: Gracia, Samuel Merryisha Sweety
Published: (2020)

Aerodynamic performance of a naca 23012 half wing model with a reverse delta wing type add-on device
by: Asrar, Waqar, et al.
Published: (2015)

Parametric investigation on the aerodynamic characteristic of NACA2415 airfoil at low reynolds number
by: Muhammad Hafizuddin, Ismail
Published: (2013)

Parametric study of NACA 4-series airfoil designs for lift-to-drag performance
by: Romli, Fairuz Izzuddin, et al.
Published: (2024)

Research onFlows for NACA 2412 airfoil using computational Fluid dynamics method
by: Kharulaman, Liyana, et al.
Published: (2019)

Comparing the effect of different turbulence models on the CFD predictions of NACA0018 airfoil aerodynamics
by: Khan, Sher Afghan, et al.
Published: (2020)

Numerical and experimental study of leading edge tubercles with vortex generators on NACA 4415 airfoil
by: Aftab, Syed Mohammed Aminuddin
Published: (2017)

Lift enhancement of NACA 4415 airfoil using biomimetic shark skin vortex generator
by: Zulkefli, Nur Faraihan, et al.
Published: (2019)

A comparative study of turbulence models on aerodynamics characteristics of a NACA0012 airfoil
by: Sadikin, Azmahani, et al.
Published: (2018)

Analisis Kitaran Melalui Kerajang Airfoil NACA (Lapisan Sempadan) Dan Kawasan Pusaran
by: Md. Ali, Affandy
Published: (2000)

Computational fluid dynamic simulation study on NACA 4412 airfoil with various angle of attacks
by: Abdul Mukhti, Muhammad Ammar Qayyum, et al.
Published: (2021)

CFD analysis of NACA4415 airfoil with γ−Reθ model considering natural transition
by: Islam, Mazharul, et al.
Published: (2015)

Numerical study of wind-tunnel wall effects on lift and drag characteristics of NACA 0012 airfoil
by: Abobaker, Mostafa, et al.
Published: (2020)

Enhanced aerodynamic performance of NACA 0009 morphing airfoil: a study on camber morphing and vortex generators
by: Dol, Sharul Sham, et al.
Published: (2025)

Characterization And Testing Of PIV Illumination System Using High Power Led On Naca 0018 Airfoil At Low Reynolds Number
by: Lai, Hoong Chuin
Published: (2018)

Study on start-up characteristics of H-Darrieus vertical axis wind turbines comprising NACA 4-digit series blade airfoils
by: Asr, Mahdi Torabi, et al.
Published: (2016)

Computation of airfoil boundary layer
by: Nurfhaizatul Aqma, Chik Aik
Published: (2007)

Induced rolling moment for NACA4412 plain and flapped wing
by: Elsayed, Omer Ali, et al.
Published: (2010)

Numerical Solutions of the Aligned Magnetic Field on the Boundary Layer Flow and Heat Transfer over a Stretching Sheet by using Keller-box Method
by: Nur Syamilah, Arifin, et al.
Published: (2016)

Effect of external acoustic excitation on NACA0015 discrete tonal noise
by: Andan, Amelda Dianne, et al.
Published: (2018)

Numerical Solutions on Mixed Convection Boundary Layer and Heat Transfer of Jeffrey Fluid over a Horizontal Circular Cylinder by using Keller-box Method
by: Syazwani, Mohd Zokri, et al.
Published: (2016)

The parallelization of the Keller box method on heterogeneous cluster of workstations
by: Hamzah, Norhafizah, et al.
Published: (2008)

LBM-LES modelling of low-Reynolds number turbulent flow over NACA0012 aerofoil
by: Nadim, Nima, et al.
Published: (2016)

Effect of Stall Strip Position, Size and Geometry on the Lift Coefficient of NACA 001 Aerofoil
by: Wee, Tee, et al.
Published: (2017)

Leading-edge flow separation control over a NACA 0012 aerofoil with DBD plasma actuators
by: Song, Longfei
Published: (2018)

Effects of bio-inspired surface roughness on a swept back tapered NACA 4412 wing
by: Malik, Khurshid, et al.
Published: (2019)

Unsteady Pressure Measurement Of NACA 0018 Undergoing Pure Pitching Motion At Different Pitch Amplitudes
by: Tong, Chee Kent
Published: (2017)

Parallelization of iterative and direct schemes for Keller-Box method on distributed memory platform
by: Alias, Norma, et al.
Published: (2010)

Aerodynamic Profile Modification of a NACA 0012 Aerofoil for Enhanced Lift-Drag Characteristics at Low Reynolds Number
by: Krishnan, Anupam, et al.
Published: (2022)

UAV NACA4415 wing structural performance analysis subjected to external aerodynamic load using Schrenk’s approximation
by: Basri, Ernnie Illyani, et al.
Published: (2019)

Performance analysis of composite ply orientation in aeronautical application of unmanned aerial vehicle (UAV) NACA4415 wing
by: Basri, Ernnie Illyani, et al.
Published: (2019)

Friedlander-Keller ray expansions and scalar wave reflection at canonically-perturbed boundaries
by: Tew, R.H.
Published: (2018)