Development of a Variable Mach Number Sliding Block Nozzle and Evaluation in the Mach 1.3 to 4.0 Range

doi 10.21236/ad0075870
Full Text
Abstract

Available in full text

Date
Authors
Publisher

Defense Technical Information Center

Related search

A Preconditioned Arbitrary Mach Number Scheme Applied to Rotating Machinery

2010English

Transition to Turbulence in Shock-Driven Mixing: A Mach Number Study

Journal of Fluid Mechanics
Mechanics of MaterialsCondensed Matter PhysicsMechanical Engineering
2011English

Control of Nozzle Flow Using Microjets at Supersonic Mach Regime

International Journal of Engineering, Transactions A: Basics
Engineering
2019English

Control of CD Nozzle Flow Using Microjets at Mach 2.1

International Journal of Innovative Technology and Exploring Engineering
Mechanics of MaterialsElectronic EngineeringCivilStructural EngineeringElectricalComputer Science
2019English

Explicit Inversion of Stodola’s Area-Mach Number Equation

Journal of Heat Transfer
Mechanics of MaterialsMaterials ScienceCondensed Matter PhysicsMechanical Engineering
2011English

Numerical Simulation on Supersonic-Flow Chemical Oxygen-Iodine Laser Adopting High Mach-Number Ramp-Nozzle Array

JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
2007English

MAESTROeX: A Massively Parallel Low Mach Number Astrophysical Solver

Journal of Open Source Software
2019English

The Density Variance–mach Number Relation in Supersonic, Isothermal Turbulence

Astrophysical Journal Letters
AstrophysicsAstronomyPlanetary ScienceSpace
2010English

1981 Calibration of the AEDC-PWT Aerodynamic Wind Tunnel (4T) at Mach Numbers From 0.1 to 1.3

1982English

Amanote Research

Note-taking for researchers

Follow Amanote

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

Privacy PolicyRefund Policy