Jessica Jungclaus, Autor bei Simuneer

Masten Space Systems: Reactive flow and heat transfer optimisation for reusable spacecraft

Masten Space Systems is using Fidelity Flow Solver, Cadence’s unstructured multi-purpose CFD solver package – for the design and analysis of various elements of reusable spacecraft and lunar vehicles.

Masten Space Systems: Reactive flow and heat transfer optimisation for reusable spacecraft

ANF Generic Missile – from subsonic to high supersonic

From Mach 0.5 to 5.0: a comparison of CFD to wind tunnel and free flight tests on the ANF, a generic missile, investigating grid dependency and numerical schemes.

Prediction of the resistance curve of a planing hull Fidelity Marine Marintek

For the prediction of the resistance curve of a planing hull and validation against model tests, Marintek used Fidelity Marine and Hexpress in this user case.

Masten Space Systems: Reactive flow and heat transfer optimisation for reusable spacecraft

Masten Space Systems: Reactive flow and heat transfer optimisation for reusable spacecraft

Masten Space Systems: Reactive flow and heat transfer optimisation for reusable spacecraft

Masten Space Systems: Reactive flow and heat transfer optimisation for reusable spacecraft

Masten Space Systems: Reactive flow and heat transfer optimisation for reusable spacecraft

Masten Space Systems: Reactive flow and heat transfer optimisation for reusable spacecraft

Author: Jessica Jungclaus

Masten Space Systems: Reactive flow and heat transfer optimisation for reusable spacecraft

ANF Generic Missile – from subsonic to high supersonic

Prediction of the resistance curve of a planing hull Fidelity Marine Marintek