Calculation of Transonic Flow around Axisymmetric Inlets

Author:

Arlinger B. G.1

Affiliation:

1. Aerospace Division, SAAB-SCANIA AB, Linkoping, Sweden

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

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1. An Ejector Air Intake Design Method for a Novel RBCC Rocket Nozzle;45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2009-08-02

2. Transonic flow computations using nonlinear potential methods;Progress in Aerospace Sciences;2000-01

3. Computational fluid dynamics based three-dimensional turbofan inlet/fan cowl analysis system;Journal of Propulsion and Power;1992-01

4. Euler flow analysis of turbine powered simulator and fanjet engine;Journal of Propulsion and Power;1991-11

5. CFD-based 3D turbofan nacelle design system;Flight Simulation Technologies Conference and Exhibit;1990-08-17

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