Author: Richard L. Perry (CAPT, USAF.)Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 150
Book Description
An Experimental Investigation of the Aerodynamic Characteristics of a Thin Supercritical Airfoil with Small Leading Edge Radius
Author: Richard L. Perry (CAPT, USAF.)Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 150
Book Description
Technical Abstract Bulletin
Author: Notices of Changes in Classification, Distribution and Availability
Author: Report
Author: NASA Supercritical Airfoils
Author: Charles D. HarrisPublisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 80
Book Description
Scientific and Technical Aerospace Reports
Author: Index of NACA Technical Publications
Author: United States. National Advisory Committee for AeronauticsPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 258
Book Description
NASA SP.
Author: Experimental Investigation Base Pressure on Blunt-trailing-edge Wings at Supersonic Velocities
Author: Dean R. ChapmanPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 852
Book Description
The pressres acting on the base of blunt-trailing-edge airfoils have been measured at Mach numbers of 1.25, 1.5, 2.0, and 3.1 and at Reynolds numbers from 0.2 to 3.8 million. Data are presented for 29 profiles both with laminar and with turbulent boundary layers approaching the trailing edges of the wings. The base pressure is found to be a function primarily of Mach number and the ratio of the boundary layer thickeness at the trailing edge to the trailing-edge thickness.
Report - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for AeronauticsPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 996
Book Description