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RAKETENANTRIEB
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Impact of chemical modeling on the numerical analysis of a LOx/GCH4 rocket engine pintle injector
Superior Al90Mg10-Based Composite Fuel Grain for a Hybrid Rocket Engine
Multiphysics Modeling for Combustion Instability in Paraffin-Fueled Hybrid Rocket Engines
General Burnback Analysis for Anisotropic and Heterogeneous Solid Propellants
Enhancing Hybrid Rocket Engine Regression Rates: The Stepped Helix Design
Computational Analysis and Regression Laws for Nozzle Erosion Prediction in Hybrid Rockets
Model for Combustion Instability in Hybrid Rocket Engines Burning Liquefying Fuels
Effect of Incoming Boundary Layer Thickness on the Flow Characteristics of a Supersonic Air Intake
A Geometrical-Irregular Boundary Layer Suction Method for Hypersonic Flow Distortion Suppression
Advanced Parametric Lobe Mixer Concepts for Internally Mixed Nozzles
Design and Investigation of Busemann Intakes for High-Speed Propulsion Systems
Design Optimization of a Novel Boundary Layer Diverter for Semi-Submerged Inlets
Supersonic External-Compression Inlets for Mach 1.4 to 2.0
Characterization of Unsteady Distortion Events for S-Duct Intakes Under Non-Uniform Inlet Conditions
Heat Transfer Augmentation with Pin Fins in the Entry Region of Circular Channels
Comparison of Engine Models of UHBPR Turbofan at High Incidence