Theory of Wing Sections


Book Description

Concise compilation of subsonic aerodynamic characteristics of NACA wing sections, plus description of theory. 350 pages of tables.







Theory of Wing Sections


Book Description




NASA Technical Report


Book Description







Turbulent Boundary-layer Temperature Recovery Factors in Two-dimensional Supersonic Flow


Book Description

An analytical method is presented for obtaining turbulent temperature recovery factors for a thermally insulated surface in supersonic flow. The method is an extension of Squire's analysis for incompressible flow. The boundary layer velocity profile is represented by a power law and a similarity is postulated for squared-velocity the static-temperature-difference profiles.







Technical Note


Book Description




Report


Book Description