HERALD OF LENINGRAD UNIVERSITY; MATHEMATICS, MECHANICS, AND ASTRONOMY SERIES (SELECTED ARTICLES).
Abstract
By successive linearization of the equations for flow past conical wings an approximate solution for them is obtained, based on the possibility of reducing the linearized system to a wave equation. An approximate analytical solution is constructed for the system of ordinary differ ential equations for flow past specially shaped wings called developable wings. It is assumed that the gas is free of internal friction forces. The motion is assumed to be steady-state and adiabatic. The solution to the aforementioned equations is obtained taking into account quan tities of the fourth order of smallness for thin, weakly curved, developable wings situated at a small angle of attack when the flow condition and the conditions at the attached discontinuity surfaces on the leading edge are satisfied. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 03, 1963
- Accession Number
- AD0413600
Entities
Organizations
- National Air and Space Intelligence Center