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(CSV)
Filters
Language:
  • Funder (1)
  • Project (4)
  • Publication Date (6)
  • Access Mode (3)
  • Type (5)
  • Language (1)
  • Content Provider (13)
  • Collected From (13)
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1,040 publications, page 1 of 104
  • Other literature type Eng UNKNOWN
    SOLLER, Sebastian; KAUFMANN, Volker; LAITHIER, Frederic;
    (2017)
    Publisher: Proceedings of the 7th European Conference for Aeronautics and Space Sciences. Milano, Italy, 3-6 july 2017
    As other aerospace companies worldwide, Airbus Safran Launchers is developing injectors for its current and future liquid rocket engines using additive manufacturing. In order to introduce this new manufacturing technology without compromise on reliability on existing e...
  • Other literature type Eng UNKNOWN
    FRANZE, Marius;
    (2017)
    Publisher: Proceedings of the 7th European Conference for Aeronautics and Space Sciences. Milano, Italy, 3-6 july 2017
    This work compares the principle of a basic fin-controlled sounding rocket with coupled computational fluid dynamic and rigid body dynamic simulations of two coupling environments: a low-fidelity approach using Missile DATCOM as semi-empirical aerodynamic solver, and a ...
  • Other literature type Eng UNKNOWN
    RIAUD, N.; BOUST, B.; BELLENOUE, M.;
    (2019)
    Publisher: Proceedings of the 8th European Conference for Aeronautics and Space Sciences. Madrid, Spain, 1-4 july 2019
    The present study focuses on the atomization and combustion of sprays generated by an unlike triplet injector, using hydrogen peroxide as oxidizer in association with ethanol or alkanes as fuels. Two injectors are tailored specifically for the fuels for a total flowrate...
  • Other literature type Eng UNKNOWN
    MARWEGE, Ansgar; RIEHMER, Johannes; KLEVANSKI, Josef; GULHAN, Ali; ECKER, Tobias; REIMANN, Bodo; DUMONT, Etienne;
    (2019)
    Publisher: Proceedings of the 8th European Conference for Aeronautics and Space Sciences. Madrid, Spain, 1-4 july 2019
    CALLISTO is a demonstrator for a reusable VTVL rocket. It is developed and built by DLR, JAXA, and CNES. The aerodynamics and aerothermodynamis of the vehicle are investigated at DLR. Experiments were performed in the Trisonic Wind Tunnel (TMK) at the Supersonic- and Hy...
  • Other literature type Eng UNKNOWN
    Le Pichon, Thomas; Laverdant, Alain;
    (2016)
    Publisher: ONERA
    Twenty years ago, a review listed the main challenges to overcome to accurately predict the reactive flow fields in ramjet combustion chambers. These issues were grouped into five topics: flow organization, combustion phenomena, stability and performance, unste...
  • Other literature type Eng UNKNOWN
    ALBOSTAN, Onur;
    (2017)
    Publisher: Proceedings of the 7th European Conference for Aeronautics and Space Sciences. Milano, Italy, 3-6 july 2017
    In this paper, the design of a control law is investigated in order to overcome the high angle of attack manoeuvring control problem. Both linear and nonlinear design methods are analysed with theoretical background. While, linear control laws are synthesized using eige...
  • Other literature type Eng UNKNOWN
    VANKAN, Wilhelmus;
    (2017)
    Publisher: Proceedings of the 7th European Conference for Aeronautics and Space Sciences. Milano, Italy, 3-6 july 2017
    The development of new higher efficiency turbofan aero engines requires several design enhancements that typically result in shorter and slimmer nacelles. Consequently these engines provide less space for the engine systems installation and for maintenance accessibility...
  • Other literature type Eng UNKNOWN
    LUPINI, Andrea; EPUREANU, Bogdan I.;
    (2019)
    Publisher: Proceedings of the 8th European Conference for Aeronautics and Space Sciences. Madrid, Spain, 1-4 july 2019
    Integrally bladed rotors (IBRs) are critical components of turbomachinery in the aerospace industry. The use of IBRs has been increasing recently because they provide enhanced performance and reduced weight. One of the most significant challenges posed by IBRs is their ...
  • Other literature type Eng UNKNOWN
    DURAND, Jean-Etienne; VILADEGUT, Alan; PINNA, Fabio; CHAZOT, Olivier;
    (2017)
    Publisher: Proceedings of the 7th European Conference for Aeronautics and Space Sciences. Milano, Italy, 3-6 july 2017
    In re-entry, spacecrafts require a Thermal Protection System (TPS) to withstand severe heat flux conditions on the surface. The most critical thermal load is located at the stagnation point, becoming the TPS design reference. Nevertheless, the design can be improved at ...
  • Other literature type Eng UNKNOWN
    WAXENEGGER, Gunther; RICCIUS, Jorg; ZAMETAEV, Evgeny; DEEKEN, Jan; SAND, Julia;
    (2017)
    Publisher: Proceedings of the 7th European Conference for Aeronautics and Space Sciences. Milano, Italy, 3-6 july 2017
    The paper in hand thematises a fatigue life analysis methodology for liquid rocket engines, with maiden focus on the combustion chamber. The method of analysis combines the engine cycle modelling tool EcosimPro/ESPSS with 2-d Finite Element analysis methods developed by...
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1,040 publications, page 1 of 104
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