Erratum To: Role of Inlet Reactant Mixedness on the Thermodynamic Performance of a Rotating Detonation Engine

Shock Waves - United States
doi 10.1007/s00193-016-0681-9
Full Text
Abstract

Available in full text

Date
Authors
Publisher

Springer Science and Business Media LLC

Related search

3D Problems of Rotating Detonation Wave in a Ramjet Engine Modeled on a Supercomputer

Supercomputing Frontiers and Innovations
Information SystemsComputer NetworksHardwareCommunicationsComputer Science ApplicationsArchitectureMathematicsComputational TheorySoftware
2018English

Rotating Detonation Wave Propulsion: Experimental Challenges, Modeling, and Engine Concepts

Journal of Propulsion and Power
SpacePlanetary ScienceFuel TechnologyMechanical EngineeringAerospace Engineering
2014English

Experimental and Numerical Study of the Rotating Detonation Engine in Hydrogen-Air Mixtures

2011English

Pressure Distribution and Performance Impacts of Aerospike Nozzles on Rotating Detonation Engines

2018English

A Theoretical Review of Rotating Detonation Engines

2019English

Analytical Estimation of Performance Parameters of an Ideal Pulse Detonation Engine.

Transactions of the Japan Society for Aeronautical and Space Sciences
SpacePlanetary ScienceAerospace Engineering
2003English

Performance of Rotating Cascades Under the Inlet-Distortions : 2nd Report, Performance Under the Circumferential Distortions

Bulletin of the JSME
Engineering
1981English

The Feasibility of a Rotating Detonation Wave Rocket Motor

1962English

Experimental Investigation on Performance and Emission of Ic-Engine by Modifying Inlet Manifold - A Review

International Journal of Advance Engineering and Research Development
2015English

Amanote Research

Note-taking for researchers

Follow Amanote

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

Privacy PolicyRefund Policy