A Circular Cone under an Angle of Attack in a Supersonic Flow of Gas,
Abstract
An investigation is reported of the flow around a cone at a small angle of attack by a uniform supersonic flow of an ideal gas. The problem is solved by the method of small disturbances. The present work presents a solution in the eddy layer with favorable accuracy. The desired solution is reduced in the work to quadratures. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- May 26, 1972
- Accession Number
- AD0747408
Entities
People
- Ya. G. Sapunkov
Organizations
- National Air and Space Intelligence Center