AEROHYDROMECHANIC THEORY OF WING IN A NONSTATIONARY FLOW (SELECTED PARTS)
Abstract
A formula is obtained for the power of liquid pressure on a profile situated in nonstationary motion. A mathematical theory is offered of an arrangement, proposed for reducing the rate of landing of parachute loads.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 13, 1965
- Accession Number
- AD0610791
Entities
People
- A. I. Nekrasov
Organizations
- National Air and Space Intelligence Center