Flow in a Y-Intake at Supersonic Speeds-Reference-Cited by-同舟云学术

Flow in a Y-Intake at Supersonic Speeds

Published:2016-01 Issue:1 Volume:32 Page:171-187
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Krushnarao Kotteda V. M.¹,Mittal Sanjay¹

Affiliation:

1. Department of Aerospace Engineering, Indian Institute of Technology, Kanpur, Uttar Pradesh 208 016, India

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.B35699

Reference29 articles.

1. MartinN. J.HolzhauserC. A. “An Experimental Investigation at Large Scale of Single and Twin NACA Submerged Side Intakes at Several Angles of Sideslip,” NACA RM-A9F20, 1949.

2. MartinN. J.HolzhauserC. A. “Analysis of Factors Influencing the Stability Characteristics of Symmetrical Twin-Intake Air-Induction Systems,” NACA TN-2049, 1950.

3. SeddonJ.TrebbleW. “Model Test on the Asymmetry of Airflow Occurring in Twin-Intake Systems at Subsonic Speeds,” Aeronautical Research Council Repts. and Memoranda 2910, London, 1955.

4. MossmanE. A.PfylF. A.LazzeroniF. A. “Experimental Investigation at Mach Numbers from 0 to 1.9 of Trapezoidal and Circular Side Inlets for a Fighter-Type Airplane,” NACA RM-A55D27, 1955.

5. AndersonW. E.PerkinsE. W. “Effects of Unsymmetrical Air-Flow Characteristics of Twin-Intake Air-Induction Systems on Airplane Static Stability at Supersonic Speeds,” NACA TM-X-94, 1959.

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