A numerical transformation solution procedure for closely coupled canard-wing transonic flows-Reference-Cited by-同舟云学术

A numerical transformation solution procedure for closely coupled canard-wing transonic flows

Published:1983-01-10 Issue: Volume: Page:
ISSN:
Container-title:21st Aerospace Sciences Meeting
language:
Short-container-title:

Author:

SHANKAR V.¹,GOEBEL T.²

Affiliation:

1. Rockwell International Science Center, Thousand Oaks, CA

2. Rockwell International Corp., Los Angeles, CA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1983-502

Reference12 articles.

1. Wing Interactions," AIAA Paper No. 82-0161. Also to avoear i n Journal of Aircraft.

2. 'Shankar, V. and Osher, S. "An Efficient Full Potential Implicit Method Based on Characteristics for Analysis of Supersonic Flows," AIAA Paper No, 82-0974. Also t o appear i n AlAA Journal.

3. 4Holst, T.L. "A Fast, Conservative rllgorithm for Solving the Transonic Full Potential Equation," AIAA Paper No. 79-1456.

4. SSmeltzer, D.B., Durston, D.A. and Stewart, V.R. "Wing and Canard Jet Flap Effects," Paper No. 83-0081.

Cited by 4 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Unsteady transonic flow calculations for interfering lifting surfaceconfigurations;Journal of Aircraft;1986-05

2. Unsteady transonic flow calculations for two-dimensional canard-wingconfigurations;Journal of Aircraft;1986-04

3. Unsteady transonic flow calculations for interfering lifting surfaceconfigurations;18th Fluid Dynamics and Plasmadynamics and Lasers Conference;1985-07-16

4. An assessment of PANDORA using a Canard/Wing/Body configuration;Applied Aerodynamics Conference;1983-07-13