Flow Asymmetry in a Y-Shaped Diverterless Supersonic Inlet: A Novel Finding
Author:
Affiliation:
1. Sharif University of Technology, 11365 Tehran, Iran
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference24 articles.
1. Elements of Propulsion: Gas Turbines and Rockets
2. Buzz Cycle Description in an Axisymmetric Mixed-Compression Air Intake
3. Intake Aerodynamics, Second Edition
4. Effects of Shock Wave/Boundary-Layer Interaction on Performance and Stability of a Mixed-Compression Inlet
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1. Evaluating Diverse Meta-Modeling Approaches for Predicting Performance Characteristics of a Twin Air Intake Based on Experimental Data;2024-05-02
2. Experimental investigation of a Y-shaped engine inlet at subsonic flow conditions;The Aeronautical Journal;2024-04-24
3. Comparison of the unstart/restart processes of a two-dimensional twin-duct supersonic inlet induced by the plug throttling and thermal choking at the sideslip state;Aerospace Science and Technology;2023-11
4. Numerical Simulation of a Y-Shaped Diverterless Supersonic Inlet;Journal of Aircraft;2023-07
5. Multi-Objective Optimization of Arbitrary Supersonic Intake Based on Axiomatic Design Theory using Kriging/MOGA;AIAA AVIATION 2023 Forum;2023-06-08
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