Experimental Investigation of Jet Noise Sources in a Hypersonic Nozzle at Takeoff
Author:
Affiliation:
1. Division of Mechanical Science and Technology, Gunma University, Gunma 376-8515, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J053336
Reference14 articles.
1. Design Study of Hypersonic Components for Precooled Turbojet Engine
2. Design and Fabrication of Variable Nozzle for Precooled Turbojet Engine
3. Feasibility of Aerodynamic-Tab Jet Noise Suppressors in a Hypersonic Nozzle at Takeoff
4. Thrust Measurement of a Rectangular Hypersonic Nozzle Using an Inclined Baffle Plate
5. Mean-Flow and Acoustic Characteristics of Cold Jets from a Rectangular Hypersonic Nozzle
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1. Acoustic Characteristics of Rectangular Hypersonic Mixer Ejector;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2023
2. Effect of Equivalence Ratio on Acoustic Characteristics in Pre-cooled Turbojet Engine Afterburner;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2023
3. Development of 1MHz Class High Frequency Optical Microphone and Its Application to Jet Noise Reduction Device Performance Investigation;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2022
4. A phenomenological approach to jet noise: the two-source model;Philosophical Transactions of the Royal Society A: Mathematical, Physical and Engineering Sciences;2019-10-14
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