Starting transients in second throat vacuum ejectors for high altitude testing facilities-Reference-Cited by-同舟云学术

Starting transients in second throat vacuum ejectors for high altitude testing facilities

Published:2021-06 Issue: Volume:113 Page:106687
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Bharate Ghanshyam^ORCID,Kumar R Arun^ORCID

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference30 articles.

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2. Experimental investigation of exhaust diffuser for rocket engines;Roshke,1962

3. Effects of diffuser length on the performance of ejectors without induced flow;German,1961

4. Experimental study of zero-flow ejectors using gaseous nitrogen;Jones,1960

5. R.C. German, J.H. Panesci, H.K. Clark, Zero secondary flow ejector-diffuser performance using annular nozzles, Technical Report AEDC-AEDC-TDR-62-196.

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