Design considerations for using indented surface treatments to control boundary layer separation
T Robarge, A Stark, SK Min, A Khalatov… - 42nd AIAA Aerospace …, 2004 - arc.aiaa.org
Although several studies have assessed the effectiveness of indented surface treatments for
delaying boundary layer separation, definitive design guidelines have never been …
delaying boundary layer separation, definitive design guidelines have never been …
Numerical assessment of the backward facing step for NACA 0015 airfoil using computational fluid dynamics
The objective of this work was to investigate the lift and drag characteristics of a NACA 0015
airfoil with a backward facing step. For a free stream velocity of 30m/s, the point of …
airfoil with a backward facing step. For a free stream velocity of 30m/s, the point of …
A Computational Design Approach on KFm Based Modified NACA-4415 for Better Aerodynamic Efficiency
This research portrays a numerical investigation of various aerodynamic properties of Kline-
Fogleman airfoils. This type of airfoils is mainly used for designing Unmanned Aerial …
Fogleman airfoils. This type of airfoils is mainly used for designing Unmanned Aerial …
Effect of backward facing step on the aerodynamic characteristics of NACA 0015 airfoil
MS Chowdhury, MM Mau, MI Shayok… - AIP Conference …, 2019 - pubs.aip.org
The purpose of this research is to study the lift and drag characteristics of a NACA 0015
airfoil with a backward facing step. A backward facing step on the upper surface has the …
airfoil with a backward facing step. A backward facing step on the upper surface has the …
[PDF][PDF] 1st International Conference on Advances in Science, Engineering and Robotics Technology 2019 (ICASERT 2019)
A Kabir, M Islam, BSM Rahman, MS Chowdhury… - 2022 - academia.edu
The target of this work was to explore the lift and drag attributes of a NACA 0015 airfoil with a
regressive confronting step. For a free stream speed of 30m/s, the purpose of partition was …
regressive confronting step. For a free stream speed of 30m/s, the purpose of partition was …
[PDF][PDF] Numerical Assessment of the Backward Facing Step for NACA 0015 Airfoil using Computational Fluid Dynamics
BSM Rahman - researchgate.net
The target of this work was to explore the lift and drag attributes of a NACA 0015 airfoil with a
regressive confronting step. For a free stream speed of 30m/s, the purpose of partition was …
regressive confronting step. For a free stream speed of 30m/s, the purpose of partition was …