Computation of vortex flow around a canard/delta combination-Reference-Cited by-同舟云学术

Computation of vortex flow around a canard/delta combination

Published:1984-11 Issue:11 Volume:21 Page:858-865
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Eriksson Lars-Erik¹,Rizzi Arthur¹

Affiliation:

1. FFA, The Aeronautical Research Institute of Sweden, Bromma, Sweden

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.45055

Reference6 articles.

1. 2Rizzi, A 'Damped Euler Equation Method to Compute Transonic Flow Around Wing Body Combinations ' AIAA Journal Vol 20 Qct?1982; pp13211328

2. 3Eriksson L E ,' A Study of Mesh Singularities and Their Effects on Numerical Errors ' FFATN 1984 10 1984

3. 4Eriksson L E Generation of Boundary Conforming Grids Around Wing Body Configurations Using Transfinite Interpolation AIAA Journal Vol 20 Qct 1982, pp 1313 1320

4. 5Sutton, E P , Some Observations of the Flow over a Delta Winged Model with 55 deg Leading Edge Sweep at Mach Numbers between 0 4 and 1 8, ARC R&M 3190 1960 "

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