Fast Preliminary Fluid Mechanical Analysis of Fighter Aircraft Wind Tunnel Models by Application of Grid Adaptation Techniques

Zastrow, Jonas (2020) Fast Preliminary Fluid Mechanical Analysis of Fighter Aircraft Wind Tunnel Models by Application of Grid Adaptation Techniques. NATO-AVT-324 - Multi-Disciplinary Design Approaches and Performance Assessment of Future Combat Aircraft, 2021-09-28 - 2021-09-30, online.

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Item URL in elib:

https://elib.dlr.de/140250/

Document Type:

Conference or Workshop Item (Speech)

Title:

Fast Preliminary Fluid Mechanical Analysis of Fighter Aircraft Wind Tunnel Models by Application of Grid Adaptation Techniques

Authors:

Authors	Institution or Email of Authors	Author's ORCID iD	ORCID Put Code
Zastrow, Jonas	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED

Date:

September 2020

Refereed publication:

Yes

Open Access:

Gold Open Access:

In SCOPUS:

In ISI Web of Science:

Status:

Published

Keywords:

combat aircraft model, grid adaptation, mesh refinement, vortex system, DLR-F23

Event Title:

NATO-AVT-324 - Multi-Disciplinary Design Approaches and Performance Assessment of Future Combat Aircraft

Event Location:

online

Event Type:

international Conference

Event Start Date:

28 September 2021

Event End Date:

30 September 2021

Organizer:

NATO

HGF - Research field:

Aeronautics, Space and Transport

HGF - Program:

Aeronautics

HGF - Program Themes:

fixed-wing aircraft

DLR - Research area:

Aeronautics

DLR - Program:

L AR - Aircraft Research

DLR - Research theme (Project):

L - Simulation and Validation (old)

Location:

Göttingen

Institutes and Institutions:

Institute of Aeroelasticity > Aeroelastic Experiments
Institute of Aeroelasticity > Aeroelastic Simulations

Deposited By:

Zastrow, Jonas

Deposited On:

12 Jan 2021 09:14

Last Modified:

24 Apr 2024 20:41

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