Rayleigh Flow of Two-Phase Nitrous Oxide as a Hybrid Rocket Nozzle Coolant

doi 10.15368/theses.2009.147
Full Text
Abstract

Available in full text

Date

Unknown

Authors
Publisher

Robert E. Kennedy Library, Cal Poly

Related search

Flow Analysis of Hybrid Rocket Nozzle Exhaust and Its Effects on Launch Pad and Guide Stand

International Journal of Recent Technology and Engineering
EngineeringManagement of TechnologyInnovation
2019English

Numerical Simulation of Gas-Particle Two-Phase Flow in a Nozzle With DG Method

Discrete Dynamics in Nature and Society
ModelingSimulation
2019English

Numerical Simulation of Two-Phase Critical Flow With the Phase Change in the Nozzle Tube

Journal of Power and Energy Systems
2012English

Rover Rocket Nozzle Materials.

1967English

Development of a New Coolant Supplying Nozzle for a Thin Blade for Reducing Coolant Supply

Seimitsu Kogaku Kaishi/Journal of the Japan Society for Precision Engineering
Mechanical Engineering
2007English

Assessment of Slag Accumulation in Solid Rocket Boosters: Part II, Two-Phase Flow Experiments

2006English

Experiment of Two-Dimensional Supersonic Nozzle Flow Using Visualization of Flow.

JOURNAL OF THE FLOW VISUALIZATION SOCIETY OF JAPAN
1989English

Effect of Orifice Nozzle Design and Input Power on Two-Phase Flow and Mass Transfer Characteristics

Transactions of the Korean Society of Mechanical Engineers, B
Mechanical Engineering
2016English

Hybrid Finite Volume Scheme for a Two-Phase Flow in Heterogeneous Porous Media

ESAIM: Proceedings
2012English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2024 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy