The achievements of the FSCD group during the last three years are described. For the case of nozzle flows in quiet ambience, new observations of the plume behaviour for truncated ideal nozzles are reported

Alziary de Roquefort, Thierry

Boccaletto, Luca

Frey, Manuel

Girard, Stève

Hannemann, Klaus

Lambaré, Hadrien

Perigo, David

Preuss, Axel

Reijasse, Philippe

Schwane, Richard

Stark, Ralf

English

Institute of Transport Research:Publications

A Theoretical Prediction of Resonance in Nozzle Flows.

Alziary de Roquefort: Direct Measurement of Side Loads with Transonic Buffeting.

Alziary de Roquefort: Low frequency fluctuations in separated turbulent compressible flows. AFI

Alziary de Roquefort: Unsteadiness of Flow Separation and End-effects Regime in a Thrust-Optimized Contour Rocket Nozzle.

Analysis of Ariane 5 base flow measurements

CFD Computation for Rocket Engine Start-up Simulation.

Cold flow testing of dual-bell nozzles in altitude simulation chambers. European conference for aerospace sciences (EUCASS

Correlation between Outer Flow and Internal Nozzle Pressure Fluctuations.

Etude expérimentale du couplage entre l’écoulement transsonique d’arrière-corps et les charges latérales dans les tuyères propulsives.

Experimental and Numerical Investigation of Heat Loads in Separated Nozzle Flow.

Filimon: Investigation of Transient Flow Phenomena at the

Flow Separation and Heat Transfer in High Area Ratio Nozzles.

Flow Separation Experimental Analysis in Overexpanded Subscale Rocket-Nozzles.

Flow Separation in Rocket Nozzles, a Simple Criteria.

Flow separation phenomena in subscale rocket nozzles,

Investigation of the Ariane-5 Nozzle by DES. European conference for aerospace sciences (EUCASS

Liege

Numerical investigation of transient flow phenomena in dual-bell nozzles.

Oschwald: Rocket nozzle cold-gas flow velocity measurements using laser-induced gratings. Journal of Raman Spectroscopy based on presentation at ECW2002;

References cited in this article in the order of appearance

Reijasse: Mesures de charges latérales dans les tuyères surdétendues.

Rocket Engine Nozzle Concepts.

Simulation of unsteady three dimensional separation behaviour in truncated ideal contour nozzles.

Technology Investigation for High Area Ratio Nozzle Concepts.

The Calorimeter Nozzle Programme.

Unsteady Side Loads in a Thrust-Optimized Contour Nozzle at Hysteresis Regime.

Unsteady simulation of the flow in a truncated ideal contour nozzle under free shock separation conditions.

Validation of the unstructured DLR-TAU-Code for Hypersonic Flow, AIAA 2002-3111 Further references of the FSCD group for information

Validation of Unsteady Turbulent Flow Predictions for Over-Expanded Expansion Nozzles.

Zimmermann: P6.2 Cold Gas Test facility for Simulation of Flight Conditions - Current Activities. European conference for aerospace sciences (EUCASS

Joint European Effort Towards Advanced Rocket Thrust Chamber Technology

https://elib.dlr.de/49250/1/FSCD-M%C3%BCnchen20051027final.pdf

Joint European Effort Towards Advanced Rocket Thrust Chamber Technology

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Institute of Transport Research:Publications