An exact solution to drag and mass-removal equations for a body in the atmosphere
type: Item
instance of: scholarly article
title: An exact solution to drag and mass-removal equations for a body in the atmosphere
zbMATH Open document ID: 0898.70019
author: V. P. Stulov
published in: Moscow University Mechanics Bulletin
publication date: 1997-10-14T00:00:00Z
review text: The author presents solutions of differential equations describing the drag and mass ablation for a meteorite in the atmosphere. A particular case of rectilinear trajectory is considered, and an exact solution is given in this case. Additionally, the author explains how to calculate aerodynamics coefficients and other dynamic parameters which correspond to observed meteorite trajectories.
Mathematics Subject Classification ID: 70M20
zbMATH DE Number: 1028447
zbMATH Keywords: rectilinear trajectory
zbMATH Keywords: aerodynamics coefficients
zbMATH Keywords: dynamic parameters
zbMATH Keywords: meteorite trajectories
reviewed by: Gasanbek T. Arazov
MaRDI profile type: Publication
description: scientific article; zbMATH DE number 1028447