16.07 Dynamics, Fall 2004.
Dynamics
A general method for determining optimum thrust nozzle contours for gas-particle flows.
Algebraic Approach to the Minimum-Cost Multi-Impulse Orbit-Transfer Problem
Analysis and Design of Space Vehicle Flight Control Systems. Volume II - Trajectory Equations
Analysis of a Cylindrical Specimen Heated by an Impinging Hot Hydrogen Jet
Analytic approach to determine optimal conditions for maximizing altitude of sounding rocket
A Study of Propellant Behavior at Zero Gravity Final Report
Axial Mode Shock Wave Combustion Instability in Liquid Propellant Rocket Engines
Catalyzed Combustion in Micro-Propulsion Devices - Project Status
Comment on “the ultimate limits of the relativistic rocket equation. The Planck photon rocket”
Compressible Model for Dilute Flows
Computational Fluid Dynamics Simulation of Hybrid Rockets of Different Scales
Computational Modeling of Magnetically Actuated Propellant Orientation
Determination of the attitude of a spinning rocket under thrust with statistically varied inputs.
Development of CFD Model for Augmented Core Tripropellant Rocket Engine
Elastic Stability of a Slender Bar with Free-Free Ends under Dynamic Loads
Forced Flexural Motion of a Rocket-Boosted Vehicle