Effect of Yaw Angle on the Performance Characteristics of Twin Intake Duct-Reference-Cited by-同舟云学术

Effect of Yaw Angle on the Performance Characteristics of Twin Intake Duct

Published:2017-05 Issue:3 Volume:54 Page:1211-1216
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Saha K.¹,Singh S. N.¹,Seshadri V.¹

Affiliation:

1. Indian Institute of Technology Delhi, New Delhi 110 016, India

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C033947

Reference14 articles.

1. DavisW. F.GoldsteinD. L. “Experimental Investigation at Supersonic Speeds of Twin-Scoop Duct Inlets of Equal Area. I—An Inlet Enclosing 61.5 Percent of the Maximum Circumference of the Forebody,” NACA RM-A7J27, Jan. 1948.

2. DavisW. F.GoldsteinD. L. “Experimental Investigation at Supersonic Speeds of Twin-Scoop Duct Inlets of Equal Area. II.—Effects of Slots upon an Inlet Enclosed 61.5 Percent of the Maximum Circumference of the Forebody,” NACA RM-A8C11, June 1948.

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

4. StroudJ. F. “Experimental Investigation of the Effect of Forebody Bluntness on the Pressure Recovery and Drag of a Twin-Scoop Inlet-Body Combination at Mach Numbers of 1.4 and 1.7,” NACA RM A51K14, Feb. 1952.

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