Publications
404 Entries
2015
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Updating a finite element based structural model of a small flexible aircraft , 2 Jan 2015Electronic (full-text) versionResearch output: Contribution to conferences > Paper
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Worst Case Analysis of a Saturated Gust Loads Alleviation System , 2 Jan 2015Electronic (full-text) versionResearch output: Contribution to conferences > Paper
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A Methodology to Assess Damage Tolerance of Composite Structures by FEA Simulation Technique , 2015, 41st European Rotorcraft Forum. MünchenResearch output: Contribution to book/conference proceedings/anthology/report > Conference contribution
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Analytical Viscous Flow Model and Test Validation of a Swirl Injector for Rocket Engine Application , 2015, 6th European Conference for Aeronautics and Space Sciences (EUCASS). Krakow, June 29 – July 3Research output: Contribution to book/conference proceedings/anthology/report > Conference contribution
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A Numerical Method for Blast Shock Wave Analysis of Missile Launch from Aircraft , 2015, In: International Journal of Aerospace Engineering. 2015, 10, 897213Research output: Contribution to journal > Research article
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Characterisation of TEGs Under Extreme Environments and Integration Efforts Onto Satellites , 2015, In: Journal of electronic materials. 44, p. 362-370, 9 p.Electronic (full-text) versionResearch output: Contribution to journal > Research article
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Derivation of the Planck and Fine-Structure Constant from Assis’s Gravity Model , 2015, In: Journal of advanced physics. 4, p. 219-221, 3 p.Electronic (full-text) versionResearch output: Contribution to journal > Research article
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Design and First Measurements of a Superconducting Gravity-Impulse-Generator , 2015, 51st AIAA Joint Propulsion Conference. Orlando, July 27-29Research output: Contribution to book/conference proceedings/anthology/report > Conference contribution
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Development and Testing of Electric and Advanced Propulsion Systems at TU Dresden , 2015, Proceedings of the 64th German Aerospace Congress (DGLR). Rostock, Sept. 22-24Research output: Contribution to book/conference proceedings/anthology/report > Conference contribution
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Development and Verification of a 500 N Ethanol/LOX Rocket Engine Using Oxide-Oxide Ceramic Matrix Composites , 2015, 6th European Conference for Aeronautics and Space Sciences (EUCASS). Krakow, June 29 – July 3Research output: Contribution to book/conference proceedings/anthology/report > Conference contribution