The Investigation for the Aerodynamic and Heat Transfer Characteristics of Slender Hypersonic Cones over a Wide Range of Angles of Attack.
Abstract
The problems of aerodynamic and heat transfer characteristics of slender sharp nosed hypersonic cones over a wide range of angles of attack are examined and the analytical solutions are presented. Three particular problems are studied: (1) inviscid flow characteristics of shock layer involving laminar separation in the leeward side with undisturbed free stream Mach number 7.95 and angle of attack 20 degrees for cone half angle 10 degrees, (2) attached three-dimensional compressible boundary layer over the cone, (3) aerodynamic and heat transfer characteristics of turbulent separated flow. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- May 30, 1971
- Accession Number
- AD0725606
Entities
People
- B. H. Yim
- Paul K. Chang
- R. U. Jettmar
- Russell A. Smith
- Sin K. Oh
Organizations
- The Catholic University of America