ON THE CALCULATION OF HIGH PRESSURE BALLOONS
Abstract
A general case is discussed for the determination of stre ses in the cylinder's wall and in the wire winding, possessing cylindrical anisotropies, along with calculating the effect of axial stretching on the cylinder's wall, at the expenses of gas pressure on the bottom of the balloon. It is assumed that every layer is orthotropic, upon which the anisotropic terminalsARE LOCATED ON THE CYLIN ER'S AXIS. Theoretical conclusions for a particular case regarding stresses on the surface of the cylinder's internal wall are compared with experimental data. All the reasonings will be justified for the balloon's cylindrical section, where the rim effect seems to be insignificant. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 01, 1961
- Accession Number
- AD0264507
Entities
People
- B.m. Lukyanov
Organizations
- National Air and Space Intelligence Center