Computational study of slotted winglets on aircraft wings
A Krishna, SV Shraviya, KJ Lampny… - AIP Conference …, 2022 - pubs.aip.org
A comparative analysis on winglet with and without slots on a NACA 0012 of Aspect ratio 2
wing is conducted to find the impact on growth and rollup of the wingtip vortex and its effects …
wing is conducted to find the impact on growth and rollup of the wingtip vortex and its effects …
Numerical study of leading-edge defect on the aerodynamic characteristics
M Sureshmohan, J Kumar… - AIP Conference …, 2022 - pubs.aip.org
For the past several years, great efforts have been put in to investigate the effect of sudden
damage in the wing surface on aircraft performance. Leading edge erosion and other …
damage in the wing surface on aircraft performance. Leading edge erosion and other …
Stall Delay Characteristics Study of NACA 2412 Wing with Outward Dimples.
P Manikandan, R Sudharsan… - … Journal of Vehicle …, 2022 - search.ebscohost.com
Flow separation in an aircraft is one of the ground causes of decrease in the lift and increase
in the pressure drag which eventually leads to loss of energy, vibrations in machinery and …
in the pressure drag which eventually leads to loss of energy, vibrations in machinery and …
Oil-cooler location optimization study of a pusher type turboprop aircraft using CFD simulation
PP Selvarajan, N Pillai, S Chidambaram - AIAA AVIATION 2022 Forum, 2022 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2022-3226. vid Turboprop aircraft with
pusher configurations do not have propeller slipstreams, resulting in inadequate ram air …
pusher configurations do not have propeller slipstreams, resulting in inadequate ram air …