Effects of Bleed Position on the Stability of a Supersonic Inlet-Reference-Cited by-同舟云学术

Effects of Bleed Position on the Stability of a Supersonic Inlet

Published:2016-09 Issue:5 Volume:32 Page:1153-1166
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Soltani Mohammad Reza¹,Daliri Abbas¹,Younsi Javad Sepahi²,Farahani Mohammad¹

Affiliation:

1. Sharif University of Technology, 145888 Tehran, Iran

2. Ferdowsi University of Mashhad, 91779 Mashhad, Iran

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.B36162

Reference38 articles.

1. Intake Aerodynamics, Second Edition

2. MattinglyJ.HeiserW.PrattD., Aircraft Engine Design, 2nd ed., AIAA Education Series, AIAA, Reston, VA, 2002, pp. 431–461.

3. FerriA.NucciL. M. “The Origin of Aerodynamics Instability of Supersonic Inlet at Subcritical Condition,” NACA RM L50K30, 1951.

4. FisherS. A.NealeM. C.BrooksA. J. “On the Subcritical Stability of Variable Ramp Intakes at Mach Number Around 2.0,” National Gas Turbine Establishment Rept. ARC-R/M-3711, England, Feb. 1970.

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