METHOD OF INVESTIGATING BOUNDARY LAYER IN A NEW TYPE WORKING SECTION
Abstract
A turbulent boundary layer in the presence of a longitudinal pressure gradient is studied. Obtained were distributions of velocities in free flow and in flows moving along a plate and along a pan. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Feb 09, 1962
- Accession Number
- AD0271821
Entities
People
- A.m. Mkhitaryan
- V.s. Maksimov
Organizations
- National Air and Space Intelligence Center