Innovative pylon concepts for engine-airframe integration for transonic transports-Reference-Cited by-同舟云学术

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Innovative pylon concepts for engine-airframe integration for transonic transports

Published:1989-06-12 Issue: Volume: Page:
ISSN:
Container-title:20th Fluid Dynamics, Plasma Dynamics and Lasers Conference
language:
Short-container-title:

Author:

NAIK DINESH¹

Affiliation:

1. Vigyan Research Associates, Inc., Hampton, VA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1989-1819

Reference6 articles.

1. 3Carlson.J.R., and Lamb,M. "Integration Effects of Pylon Geometry and Rearward Mounted Nacelles for a High-WingTransport." AIAA-87-1920.

2. 6Mineck. R. E., and Lawing, P. L. "High Reynolds Number Tests of the NASA SC(2)- 0012 Airfoil in the Langley 0.3 m Transonic CryogenicTunnel,NASATM 89102. July 1987.

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