Aeroptical Effects Caused by Supersonic Airflow around an Ogival Body

التفاصيل البيبلوغرافية
العنوان: Aeroptical Effects Caused by Supersonic Airflow around an Ogival Body
المؤلفون: A. A. Sukharev
المصدر: Atmospheric and Oceanic Optics. 32:207-212
بيانات النشر: Pleiades Publishing Ltd, 2019.
سنة النشر: 2019
مصطلحات موضوعية: Diffraction, Shock wave, Physics, Atmospheric Science, business.industry, Airflow, Mechanics, Computational fluid dynamics, Oceanography, Atomic and Molecular Physics, and Optics, Compressibility, Supersonic speed, Rectilinear propagation, business, Beam (structure), Earth-Surface Processes
الوصف: An optical model of a shock wave generated due to supersonic airflow around a body of an ogival form is developed. Mean values of airflow parameters were calculated from the Navier–Stokes equations using the CFD Fluent 6.0 software package accounting for the gas compressibility. It is shown that the maximum values of the structure parameters are several orders of magnitude larger than the values typical for an unperturbed shock wave in the atmosphere. Results of numerical simulation of propagation of an optical beam which crosses the shock wave at the beginning of a path and then propagates through a homogeneous medium are presented. It is shown that an increase in the aircraft speed increases the transverse dimensions of the beam due to diffraction. The angular deviation of the beam from rectilinear propagation under the impact of the shock wave depends only on the altitude above the Earth’s surface where the shock wave is generated. The impact of the shock wave on the crossing beam weakens as the altitude increases.
تدمد: 2070-0393
1024-8560
DOI: 10.1134/s1024856019020131
URL الوصول: https://explore.openaire.eu/search/publication?articleId=doi_________::ae1a021c41b237cc69783f9e90f10f6c
https://doi.org/10.1134/s1024856019020131
Rights: CLOSED
رقم الانضمام: edsair.doi...........ae1a021c41b237cc69783f9e90f10f6c
قاعدة البيانات: OpenAIRE
الوصف
تدمد:20700393
10248560
DOI:10.1134/s1024856019020131