Reduction of Base Drag during Supersonic Velocities using Power Method,
Abstract
The article describes the results of experimental drag investigation of a nacelle containing two engines and a wing of a long range supersonic plane for M = 2.4.
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 07, 1972
- Accession Number
- AD0750950
Entities
People
- B. I. Buryshev
Organizations
- National Air and Space Intelligence Center