An experimental study of 2-D mixer/ejector noise and thrust characteristics

Author:

Krasheninnikov S.1,Mironov A.1,Paulukov E.2,Zitenev V.2,Julliard J.3,Maingre E.3

Affiliation:

1. Central Inst. of Aviation Motors, Moscow, Russia

2. TsAGI, Zhukovsky, Russia

3. SNECMA, Moissy-Cramayel, France

Publisher

American Institute of Aeronautics and Astronautics

Reference15 articles.

1. Smith M.J.T., Lowrie B.W.,Brooks J.R., Bushell K.W. Future supersonic transport noise - lessons from the past. AIAA Paper 88-2989, 14p.

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1. The problems of creating a propulsion system of a new generation supersonic passenger aircraft (review);VESTNIK of Samara University. Aerospace and Mechanical Engineering;2023-05-10

2. CFD Optimization of Ejector Flaps in a One-Sided Mixer Ejector Nozzle;AIAA Scitech 2019 Forum;2019-01-06

3. Effect of multilobe ejector nozzle elements shape on the jet noise;5th AIAA/CEAS Aeroacoustics Conference and Exhibit;1999-05-10

4. Method for Noise Suppressing Nozzle Calculation and First Results of Its Implementation;Journal of Propulsion and Power;1998-01

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