Numerical investigation of supersonic inlet with realistic bleed andbypass systems-Reference-Cited by-同舟云学术

Numerical investigation of supersonic inlet with realistic bleed andbypass systems

Published:1991-01-07 Issue: Volume: Page:
ISSN:
Container-title:29th Aerospace Sciences Meeting
language:
Short-container-title:

Author:

FUJIMOTO AKIRA¹,NIWA NOBUO²,SAWADA KEISUKE³

Affiliation:

1. Kawasaki Heavy Industries, Ltd., Gifu Technical Institute, Kakamigahara, Japan

2. Kawasaki Heavy Industries, Ltd., Seishin, Japan

3. Tohoku University, Sendai, Japan

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1991-127

Reference14 articles.

1. "Research on Variable Geometry and Bleed System of High Mach Inlet, 1990n,Report of Investigations on Advanced Aircraft Technology,No.0107, the Societyof Japanese Aeronautical Companies, 1990,in Japanese.

2. "Intake Aerodynamics", Seddon, J.and Goldsmith, E.L., AIAA Education Series, 1985.

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