Optimization design of energy deposition on single expansion ramp nozzle-Reference-Cited by-同舟云学术

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Optimization design of energy deposition on single expansion ramp nozzle

Published:2017-11 Issue: Volume:140 Page:351-361
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Ju Shengjun,Yan Chao,Wang Xiaoyong,Qin Yupei,Ye Zhifei

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference44 articles.

1. NASA hypersonic flight demonstrators—overview, status, and future plans;Moses;Acta Astronaut.,2004

2. X-51 Waverider Makes Historic Hypersonic Flight;US Air Force,2010

3. Studies of scramjet/airframe integration techniques for hypersonic aircraft;Edwards;AIAA Pap.,1975

4. Scramjet Propulsion;Curran,2000

5. Scramjet engines: the first forty years;Edward;J. Propuls. Power,2001

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1. Collaborative optimization of two-dimensional convergent divergent exhaust system based on Kriging model;Physics of Fluids;2024-07-01

2. Multi-objective optimization design of scramjet nozzle based on grey wolf optimization algorithm and kernel extreme learning machine surrogate model;Physics of Fluids;2024-02-01

3. The Influence of External Flow Field on the Flow Separation of Overexpanded Single-Expansion Ramp Nozzle;Aerospace;2023-11-13

4. Fast and reliable prediction of scramjet flowfields via Gaussian process latent variable model and deep learning;Physics of Fluids;2023-04-01

5. Inverse Design of Nozzle Using Convolutional Neural Network;Journal of Spacecraft and Rockets;2022-07

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