المؤلفون: Priyadharshini Murugesan, A. R. Srikrishnan, Akram Mohammad, Ratna Kishore Velamati

المصدر: Energies, Vol 16, Iss 4, p 1762 (2023)

مصطلحات موضوعية: flow separation, heat transfer, overexpanded nozzle, Thrust Optimized Parabolic (TOP) nozzle, Technology

وصف الملف: electronic resource

Relation: https://www.mdpi.com/1996-1073/16/4/1762; https://doaj.org/toc/1996-1073

URL الوصول: https://doaj.org/article/d3847060fa4749a5b73d0908fa7f5729

المؤلفون: Priyadharshini Murugesan, Arjun Biju Kumar, Akhil Teja Kambhampati, Shashank Pillai, Girish Chandar Chandrasekar, Srikrishnan Ambattu Raghavannambiar, Ratna Kishore Velamati

المصدر: Journal of Aerospace Technology and Management, Vol 12, Iss 1 (2020)

مصطلحات موضوعية: Supersonic jet, Shock cell length, Supersonic core length, Numerical analysis., Technology, Motor vehicles. Aeronautics. Astronautics, TL1-4050

وصف الملف: electronic resource

Relation: https://www.jatm.com.br/jatm/article/view/1126; https://doaj.org/toc/2175-9146

URL الوصول: https://doaj.org/article/f3731ce26c674ee1899b8e2cdcdc40f8

المؤلفون: Shashank Pillai, Ratna Kishore Velamati, Srikrishnan Ambattu Raghavannambiar, Girish Chandar Chandrasekar, Priyadharshini Murugesan, Akhil Teja Kambhampati, Arjun Biju Kumar

المصدر: Journal of Aerospace Technology and Management, Vol 12, Iss 1, Pp 4220-4220 (2020)
Journal of Aerospace Technology and Management, Volume: 12, Article number: e4220, Published: 09 OCT 2020
Journal of Aerospace Technology and Management v.12 2020
Journal of Aerospace Technology and Management
Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
instacron:DCTA

مصطلحات موضوعية: shock cell length, numerical analysis, lcsh:Motor vehicles. Aeronautics. Astronautics, Nozzle, Aerospace Engineering, 02 engineering and technology, 01 natural sciences, lcsh:Technology, 010305 fluids & plasmas, symbols.namesake, Supersonic core length, 0203 mechanical engineering, 0103 physical sciences, Heat capacity ratio, Supersonic speed, Shock cell length, Physics, 020301 aerospace & aeronautics, Jet (fluid), Shock (fluid dynamics), lcsh:T, Numerical analysis, supersonic jet, Mechanics, supersonic core length, Supersonic jet, Mach number, symbols, Working fluid, lcsh:TL1-4050

وصف الملف: text/html

URL الوصول: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::a81d28a90c58143692603c268adc4cb7
https://www.scielo.br/pdf/jatm/v12/2175-9146-jatm-12-e4220.pdf