Approximate analytical method of calculating the trajectories of an aircraft in the atmosphere (Q798019)
From MaRDI portal
 | This is the item page for this Wikibase entity, intended for internal use and editing purposes. Please use this page instead for the normal view: Approximate analytical method of calculating the trajectories of an aircraft in the atmosphere |
scientific article; zbMATH DE number 3870679
| Language | Label | Description | Also known as |
|---|---|---|---|
| English | Approximate analytical method of calculating the trajectories of an aircraft in the atmosphere |
scientific article; zbMATH DE number 3870679 |
Statements
Approximate analytical method of calculating the trajectories of an aircraft in the atmosphere (English)
0 references
1984
0 references
An approximate analytical method is proposed to solve the system of differential equations defining the plane motion of an aircraft in equatorial entry, with the planet rotation and the ablation of the mass of heat insulation coating from the vehicle surface taken into account. It is shown that the error of computation did not exceed 10\%.
0 references
high density atmosphere
0 references
motion of an aircraft
0 references
planet rotation
0 references
heat insulation
0 references
