In Silico Studies on Truncated Aerospike Nozzle with Optimum Cowl Length for Single Stage to Orbit Vehicles-Reference-Cited by-同舟云学术

In Silico Studies on Truncated Aerospike Nozzle with Optimum Cowl Length for Single Stage to Orbit Vehicles

Published:2023-05-27 Issue: Volume: Page:
ISSN:
Container-title:25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
language:
Short-container-title:

Author:

Sundaria Shubhangi¹,Bhagat Amritansh Kumar¹,Sanal Kumar VR²

Affiliation:

1. Amity University

2. Vikram Sarabhai Space Centre

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2023-3105

Reference52 articles.

1. V.R.SanalKumaretal."Thetheoreticalpredictionoftheboundarylayerblockageandexternal flowchokingatmoving aircraft in ground effects,"PhysFluids33(2021),

2. Verma SB. Performance characteristics of an annular conical aerospike nozzle with freestream effect. Journal of Propulsion and Power. 2009May;25(3):783-91.

3. Study of Conical Aerospike Nozzles with Base-Bleed and Freestream Effects

4. NairPP,SuryanA,KimHD.Computationalstudyofperformancecharacteristicsfortruncatedconicalaerospikenozzles. Journalof Thermal Science. 2017Dec;26:483-9.

5. RezaMS,AroraK.Contourdesignofaerospikenozzleandcomparisonofperformance.In2017InternationalConference on Infocom Technologies and Unmanned Systems (Trends and Future Directions)(ICTUS) 2017 Dec 18 (pp. 836-842). IEEE.

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Diagnostic Investigation of Fluid Flow Characteristics of Aerospike Nozzles During Streamtube Compression and Shock Wave Generation at Various Pressure Ratios;AIAA AVIATION 2023 Forum;2023-06-08