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

المصدر: Journal of Aerospace Technology and Management. January 2020 12

مصطلحات موضوعية: Supersonic jet, Shock cell length, Supersonic core length, Numerical analysis

وصف الملف: text/html

URL الوصول: http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462020000100340

المؤلفون: A.K., Mubarak, P.S., Tide

المصدر: Aircraft Engineering and Aerospace Technology, 2018, Vol. 91, Issue 1, pp. 145-156.

URL الوصول: http://www.emeraldinsight.com/doi/10.1108/AEAT-12-2017-0275

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: Thillaikumar T., Tamal Jana, Mrinal Kaushik

المصدر: Actuators; Volume 9; Issue 3; Pages: 88

مصطلحات موضوعية: centerline pressure decay, pressure profile, shadowgraph technique, shock-cell length, jet mixing, noise attenuation

وصف الملف: application/pdf

Relation: Miniaturized and Micro Actuators; https://dx.doi.org/10.3390/act9030088

الاتاحة: https://doi.org/10.3390/act9030088

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

المؤلفون: Kazuyasu MATSUO, Masashi KASHITANI, Mitsuharu MASUDA, Yoshiaki MIYAZATO

المصدر: JSME International Journal Series B Fluids and Thermal Engineering. 1998, 41(2):375

المؤلفون: Hiroshi Katanoda, Kazuyasu Matsuo, Mitsuharu Masuda, Yoshiaki Miyazato, 宮里 義昭, 松尾 一泰, 片野田 洋, 益田 光治

المصدر: 日本機械学会論文集 B編 / Transactions of the Japan Society of Mechanical Engineers Series B. 1995, 61(589):3236