Overview and summary of the third AIAA high lift prediction workshop

CL Rumsey, JP Slotnick, AJ Sclafani - Journal of Aircraft, 2019 - arc.aiaa.org
The Third AIAA CFD High Lift Prediction Workshop was held in Denver, Colorado, in June
2017. The goals of the workshop continued in the tradition of the first and second high-lift …

Computational aerodynamic investigation of long strake-tail missile configurations

M Ghoreyshi, A Jirasek, P Aref, J Seidel - Aerospace Science and …, 2022 - Elsevier
The efforts for the computational investigation and validation of different Missile
Configurations tested at the US Air Force Academy are summarized. The missile …

Vortex Interaction Characteristics of Multiswept Wings at Subsonic Speeds

M Ghoreyshi, C Fagley, J Seidel - AIAA Journal, 2023 - arc.aiaa.org
Despite the sufficient knowledge on the physics of vortices formed over slender delta wings,
there is a lack of understanding about how corotating and counter-rotating vortices near the …

Computational investigation of quiet propeller designs for small unmanned aerial vehicles

M Ghoreyshi, P Aref, CF Wisniewski, J Seidel… - Aerospace Science and …, 2023 - Elsevier
The noise produced by the propellers of micro Unmanned Air Vehicles (UAVs) could be
counterproductive to their mission, since adversaries can often hear them from a distance …

Aerodynamic Characteristics of Circular and Noncircular Cross-Sectional Missile Configurations

M Ghoreyshi, NM Shumway, P Aref, A Jirasek… - Journal of Spacecraft …, 2024 - arc.aiaa.org
This paper summarizes an investigation of the aerodynamic performance of missile
configurations with axisymmetric and nonaxisymmetric cross sections. Configurations have …

Aerodynamic flow field analysis of vortex interactions on multi-swept wing configurations

M Ghoreyshi, C Fagley, J Seidel - Aerospace Science and Technology, 2024 - Elsevier
The underlying flow physics of vortex breakdown and vortex-vortex interactions at moderate
to high angles of attack is not well understood. This lack of understanding is a challenge to …

Experimental and numerical comparison of different missile body cross sectional shapes

N Shumway, M Ghoreyshi - AIAA SCITECH 2023 Forum, 2023 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2023-0055. vid How body shapes effect
the forces produced has been studied for small angle of attack ranges or tapered bodies, but …

Aerodynamic characterization of noncircular cross-section missile configurations

M Ghoreyshi, P Aref, N Shumway, J Seidel - Aerospace Science and …, 2024 - Elsevier
This article summarizes the computational efforts in the aerodynamic characterization of new
missile configurations designed at the US Air Force Academy that have either circular, or …

Design Perspectives of a System Identification Approach of the NATO AVT-316 Multi-Swept Wing Aerodynamics

M Ghoreyshi, P Aref, J Seidel - Aerospace Science and Technology, 2024 - Elsevier
Air supremacy requires enhanced maneuvering capabilities at high angles of attack and
even beyond the stall angle. High angle-of-attack (high-α) maneuverability can be achieved …

Evaluation of Reduced Order Aerodynamic Models for Transonic Flow Over a Multiple-Swept Wing Configuration

M Ghoreyshi, P Aref, M Stradtner, M van Rooij… - … FORUM AND ASCEND …, 2024 - arc.aiaa.org
Efficient input data generation for reduced-order model applications to accurately predict
aerodynamic performance and stability characteristics over a large part of a fighter aircraft's …