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Experiments on aerothermoelastic fluid–structure interaction in hypersonic flow

Journal of sound and vibration, 2022-08, Vol.531, p.116714, Article 116714

2022

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Aerodynamic characteristics of the retro propulsion landing burn of vertically landing launchers

Experiments in fluids, 2024-08, Vol.65 (8), Article 115

2024

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Velocity measurements in particle-laden high-enthalpy flow using non-intrusive techniques

Experiments in fluids, 2024-03, Vol.65 (3), Article 39

2024

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Mixed Oxide Aerogels with High‐Performance Insulating Properties for High‐Temperature Space Application

Advanced engineering materials, 2023-11, Vol.25 (21)

2023

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On the subsonic near-wake of a space launcher configuration with exhaust jet: Experimental investigation by means of particle image velocimetry (PIV) on the subsonic (Mach 0.5–0.9) near-wake flow of a space launcher configuration with a cold, over-expanded, supersonic jet

Experiments in fluids, 2019-11, Vol.60 (11), Article 165

2019

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Aerodynamic interactions of blunt bodies free-flying in hypersonic flow

Experiments in fluids, 2024-06, Vol.65 (6), Article 80

2024

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Particle mass flow determination in dust-laden supersonic flows by means of simultaneous application of optical measurement techniques

Experiments in fluids, 2023-03, Vol.64 (3), Article 49

2023

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Shock interaction induced heat flux augmentation in hypersonic flows

Experiments in fluids, 2021-12, Vol.62 (12), Article 242

2021

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Simultaneous determination of particle size, velocity, and mass flow in dust-laden supersonic flows

Experiments in fluids, 2022-04, Vol.63 (4), Article 64

2022

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Experiments on a smooth wall hypersonic boundary layer at Mach 6

Experiments in fluids, 2018-04, Vol.59 (4), p.1-21, Article 68

2018

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Martian flow characterization using tunable diode laser absorption spectroscopy, in high enthalpy facilities

Acta astronautica, 2023-12, Vol.213, p.204-214

2023

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On subsonic near-wake flows of a space launcher configuration with various base geometries

Experiments in fluids, 2021-06, Vol.62 (6), Article 122

2021

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Capsule aerodynamics and shock-wave boundary layer interaction (SBLI) in supersonic and transonic flow

Experiments in fluids, 2022-03, Vol.63 (3), Article 61

2022

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A study on heat flux predictions for re-entry flight analysis

Acta astronautica, 2021-10, Vol.187, p.271-280

2021

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Plume and wall temperature impact on the subsonic aft-body flow of a generic space launcher geometry

Experiments in fluids, 2024, Vol.65 (8)

2024

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Experiments on the effect of laminar–turbulent transition on the SWBLI in H2K at Mach 6

Experiments in fluids, 2015-03, Vol.56 (3), Article 49

2015

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Interactions between asteroid fragments during atmospheric entry

Icarus (New York, N.Y. 1962), 2020-02, Vol.337, p.113468, Article 113468

2020

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Improved representation of destructive spacecraft re-entry from analysis of high enthalpy wind tunnel tests of spacecraft and equipment

Acta astronautica, 2019-11, Vol.164, p.287-296

2019

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Aerodynamics of inclined cylindrical bodies free-flying in a hypersonic flowfield

Experiments in fluids, 2021-09, Vol.62 (9), Article 182

2021

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Longitudinal stability measurements of a winged biconic configuration in supersonic flow

Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering, 2022-03, Vol.236 (3), p.457-467

2022

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Thermal Qualification of the UHTCMCs Produced Using RF-CVI Technique with VMK Facility at DLR

Journal of composites science, 2022-01, Vol.6 (1), p.24

2022

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Experimental results on unsteady shock-wave/boundary-layer interaction induced by an impinging shock

CEAS space journal, 2016-03, Vol.8 (1), p.3-12

2016

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Development of an intrusive technique for particles collection in rockets plume

Acta astronautica, 2019-05, Vol.158, p.361-374

2019

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Design of converging-diverging nozzles with constant-radius centerbody

CEAS space journal, 2020-06, Vol.12 (2), p.191-201

2020

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Experimental investigation of hot and cold side jet interaction with a supersonic cross-flow

Aerospace science and technology, 2009-12, Vol.13 (8), p.488-496

2009

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Experiments on aerothermoelastic fluid–structure interaction in hypersonic flow

Aerodynamic characteristics of the retro propulsion landing burn of vertically landing launchers

Velocity measurements in particle-laden high-enthalpy flow using non-intrusive techniques

Mixed Oxide Aerogels with High‐Performance Insulating Properties for High‐Temperature Space Application

On the subsonic near-wake of a space launcher configuration with exhaust jet: Experimental investigation by means of particle image velocimetry (PIV) on the subsonic (Mach 0.5–0.9) near-wake flow of a space launcher configuration with a cold, over-expanded, supersonic jet

Aerodynamic interactions of blunt bodies free-flying in hypersonic flow

Particle mass flow determination in dust-laden supersonic flows by means of simultaneous application of optical measurement techniques

Shock interaction induced heat flux augmentation in hypersonic flows

Simultaneous determination of particle size, velocity, and mass flow in dust-laden supersonic flows

Experiments on a smooth wall hypersonic boundary layer at Mach 6

Martian flow characterization using tunable diode laser absorption spectroscopy, in high enthalpy facilities

On subsonic near-wake flows of a space launcher configuration with various base geometries

Capsule aerodynamics and shock-wave boundary layer interaction (SBLI) in supersonic and transonic flow

A study on heat flux predictions for re-entry flight analysis

Plume and wall temperature impact on the subsonic aft-body flow of a generic space launcher geometry

Experiments on the effect of laminar–turbulent transition on the SWBLI in H2K at Mach 6

Interactions between asteroid fragments during atmospheric entry

Improved representation of destructive spacecraft re-entry from analysis of high enthalpy wind tunnel tests of spacecraft and equipment

Aerodynamics of inclined cylindrical bodies free-flying in a hypersonic flowfield

Longitudinal stability measurements of a winged biconic configuration in supersonic flow

Thermal Qualification of the UHTCMCs Produced Using RF-CVI Technique with VMK Facility at DLR

Experimental results on unsteady shock-wave/boundary-layer interaction induced by an impinging shock

Development of an intrusive technique for particles collection in rockets plume

Design of converging-diverging nozzles with constant-radius centerbody

Experimental investigation of hot and cold side jet interaction with a supersonic cross-flow

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