AES4AC NEWS

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Date

News

Q4 2024
Q3 2024

!!REPORT IN PREPARATION!!
Prediction and analysis of
subsonic & supersonic(hypersonic)
steady & unsteady
aerodynamics,
free surface hydrodynamics &
aeroacoustics

for oscillating and deforming air/water vehicles.

An introduction, installation & user guide to

the gradient free boundary volume method
AES=O=

!!REPORT IN PREPARATION!!

Q3 2023

Installation and compact userguide of AES=3= is available report.pdf

Q4 2022

AES=2= extented with supersonic/hypersonic modelling accounting for true geometry

Piston theories implicit/explicit accounting for thickness
Propiertor nearly exact wedge treatment.

Hypersonic.pdf

Q4 2021

AES=3= extented with supersonic/hypersonic modelling accounting for true geometry

Piston theories implicit/explicit accounting for thickness

Hypersonic.pdf

starship

Q2 2021

Report: Meshing Around with AES=V=

Q1 2020

Report: Aeroelastic Application of AES=V=

Q1 2016

Report: An Application of AES=3=

Q3 2019

AES=V= extented with time traces and flutter analysis

An aero(-servo-)elastic pre and post processor

Q1 2019

AES=V= extented with grid generation facilities

August 2017

Low cost straightforward and easy to use visualization app AES=V= introduced

December 2016

AES=O= extented with acoustic modelling. Easy modeling of incident sound potential & impedance distributions.

November 2016

AES=O= extented with efficient linearised free surface Havelock(implicit) and Rankine (explicit) modelling for oscillating lifting and nonlifting watercraft configurations at zero and non-zero Froude numbers