Postscript for Special Issue "Advances in Hybrid Rocket Technology and Related Analysis Methodologies" von Carmicino, Carmine

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Special Issue “Hybrid Rocket (Volume II)” von Shimada, Toru, Carmicino, Carmine, Karabeyoglu, Arif

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Model for Combustion Instability in Hybrid Rocket Engines Burning Liquefying Fuels von Gallo, Giuseppe, Carmicino, Carmine

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The Application of Computational Thermo-Fluid-Dynamics to the Simulation of Hybrid Rocket Internal Ballistics with Classical or Liquefying Fuels: A Review von Di Martino, Giuseppe Daniele, Carmicino, Carmine, Mungiguerra, Stefano, Savino, Raffaele

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Modeling of High Density Polyethylene Regression Rate in the Simulation of Hybrid Rocket Flowfields von Bianchi, Daniele, Leccese, Giuseppe, Nasuti, Francesco, Onofri, Marcello, Carmicino, Carmine

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Acoustic Excitation as Triggering Mechanism of the “DC Shift” in Hybrid Rockets von Carmicino, Carmine, Pastrone, Dario

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Advances in Hybrid Rocket Technology and Related Analysis Methodologies

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Special Issue “Advances in Hybrid Rocket Technology and Related Analysis Methodologies” von Carmicino, Carmine

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Self-consistent surface-temperature boundary condition for liquefying-fuel-based hybrid rockets internal-ballistics simulation von Carmicino, Carmine, Gallo, Giuseppe, Savino, Raffaele

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Novel Comprehensive Technique for Hybrid Rocket Experimental Ballistic Data Reconstruction von Carmicino, Carmine, Pastrone, Dario

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Prediction of the fuel regression-rate in a HDPE single port hybrid rocket fed by liquid nitrous oxide von Gallo, Giuseppe, Kamps, Landon, Hirai, Shota, Carmicino, Carmine, Harunori, Nagata

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Hybrid Rockets with Axial Injector: Port Diameter Effect on Fuel Regression Rate von Bianchi, Daniele, Nasuti, Francesco, Carmicino, Carmine

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One-dimensional modelling of the nozzle cooling with cryogenic oxygen flowing through helical channels in a hybrid rocket von Gallo, Giuseppe, Kamps, Landon, Hirai, Shota, Carmicino, Carmine, Nagata, Harunori

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Reconstructed Ballistic Data Versus Wax Regression-Rate Intrusive Measurement in a Hybrid Rocket von Messineo, Jerome, Kitagawa, Koki, Carmicino, Carmine, Shimada, Toru, Paravan, Christian

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Analytical modeling of the one-dimensional acoustic field in hybrid rocket combustion chamber von Carmicino, Carmine, Di Martino, Giuseppe D.

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Evaluation of Radiative Heat-Transfer Effect on Paraffin-Wax Regression Rate in Hybrid Rocket von Naka, Genya, Carmicino, Carmine, Messineo, Jérôme, Kitagawa, Koki, Shimada, Toru

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Simulation of Gaseous Oxygen/Hydroxyl-Terminated Polybutadiene Hybrid Rocket Flowfields and Comparison with Experiments von Bianchi, Daniele, Betti, Barbara, Nasuti, Francesco, Carmicino, Carmine

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Analysis of Acoustics and Vortex Shedding Interactions in Hybrid Rocket Motors von Pastrone, Dario, Casalino, Lorenzo, Carmicino, Carmine

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A simplified computational fluid-dynamic approach to the oxidizer injector design in hybrid rockets von Di Martino, Giuseppe D., Malgieri, Paolo, Carmicino, Carmine, Savino, Raffaele

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Role of Injection in Hybrid Rockets Regression Rate Behaviour von Carmicino, Carmine, Sorge, Annamaria Russo

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