Numerical simulation of two-dimensional inlet flowfields
Author:
Affiliation:
1. Old Dominion University, Norfolk Virginia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.48254
Reference10 articles.
1. Beam R and Warming R F An Implicit Finite Difference Algorithm for Hyperbolic Systems in Conservation Law Form Journal of Computational Physics Vol 22 Sept 1976 pp 87 100
2. D Souza N , Molder, S and Moretti G Numerical Method for Hyperbolic Internal Flow Over Blunt Leading Edges and Two Blunt Bodies AIAA Journal Vol10May 1972pp617627
3. 4Bansod P Supersonic Flow About Ducted Bodies With Subsonic Internal Boundaries AIAA Journal Vol 12 June 1975 pp.531 538
4. Knight D D Numerical Simulation of Realistic High Speed Inlets Using the Navier Stokes Equations AIAA Journal Vol 15 Nov 1977 pp 1583 1589
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1. Effect of Side Gust on Performance of External Compression Supersonic Inlet;Journal of Aircraft;2019-03
2. Performance Prediction of Internal Compression Supersonic Air Intake at Range of Mach Numbers (1.1-1.5);Tikrit Journal of Engineering Sciences;2016-08-31
3. The external drag of a simple axisymmetric body of revolution in subsonic and supersonic flow with variable mass flowthrough ratios;4th Applied Aerodynamics Conference;1986-06-09
4. Evaluation of a method for analyzing the aperture region of two-dimensional external compression inlets;Aircraft Design Systems and Operations Meeting;1985-08-17
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