Results of an improved version of LTRAN2 for computing unsteady airloads on airfoils oscillating in transonic flow-Reference-Cited by-同舟云学术

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Results of an improved version of LTRAN2 for computing unsteady airloads on airfoils oscillating in transonic flow

Published:1979-07-23 Issue: Volume: Page:
ISSN:
Container-title:12th Fluid and Plasma Dynamics Conference
language:
Short-container-title:

Author:

HOUWINK R.¹,VAN DER VOOREN J.¹

Affiliation:

1. Nationaal Lucht- en Ruimtevaartlaboratorium, Amsterdam, Netherlands

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1979-1553

Reference10 articles.

1. Implicit finite-difference computations of unsteady transonic flows about airfoils, including the treatment of irregular shock-wave motions

2. Couston, M. and Angglini, J.J. "Solution of nonsteady two-dimensional transonic small disturbances potential flow equation:' ONERA T.P.no.1978-69, 1978.

Cited by 9 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. Advances in the Understanding and Computation of Unsteady Transonic Flow;Recent Advances in Aerodynamics;1986

2. Transonic time responses of the MBB A-3 supercritical airfoil including active controls;Journal of Aircraft;1985-05

3. Transonic flutter and response analyses of two 3-degree-of-freedom airfoils;Journal of Aircraft;1982-10

4. Transonic time-response analysis of three D.O.F. conventional and supercritical airfoils;23rd Structures, Structural Dynamics and Materials Conference;1982-05-10

5. Application of Transonic Codes to Flutter Analysis of Conventional and Supercritical Airfoils;Journal of Aircraft;1982-03

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