Amanote Research

Amanote Research

    RegisterSign In

Numerical Evaluation of a Two Dimensional Pitch and Yaw Vectoring Nozzle Using an Inviscid Flow Solver

doi 10.1115/91-gt-160
Full Text
Open PDF
Abstract

Available in full text

Date

June 3, 1991

Authors
P. L. CheathamM. C. GridleyS. H. Walker
Publisher

American Society of Mechanical Engineers


Related search

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

JOURNAL OF THE FLOW VISUALIZATION SOCIETY OF JAPAN
1989English

Three Dimensional Inviscid Computation of an Impeller Flow

1983English

Performance Research of Axisymmetric Vectoring Nozzle Based on Numerical Simulations

2015English

Nonexistence of Coherent Structures in Two-Dimensional Inviscid Channel Flow

Mathematical Modelling of Natural Phenomena
ModelingApplied MathematicsSimulation
2012English

Aero-Thermal Performance of a Two Dimensional Highly Loaded Transonic Turbine Nozzle Guide Vane: A Test Case for Inviscid and Viscous Flow Computations

1990English

The Flow Through an Annular Turbine Nozzle With Nonuniform Pitch

1994English

Numerical Simulation of an Over-Expanded Supersonic Nozzle Flow

2018English

Numerical Analysis of Two-Dimensional Viscoelastic Flow

Journal of the Textile Machinery Society of Japan
1977English

Thrust Vectoring Effects of a Transverse Gas Injection Into a Supersonic Cross Flow of an Axisymmetric Convergent-Divergent Nozzle

2013English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2025 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy