Author: United States. National Advisory Committee for AeronauticsPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1262
Book Description
Technical Note - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for AeronauticsPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1262
Book Description
WADC Technical Report
Author: United States. Wright Air Development DivisionPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1430
Book Description
Technical Note
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.
AN ANALYTIC DESIGN METHOD FOR A TWO-DIMENSIONAL ASYMMETRIC CURVED NOZZLE.
Author: HANS PETER LIEPMANAn Analytic design Method for a Two-Dimensional Asymmetric Curved Nozzle June,1953
Author: H.P. LiepmanReport
Author: Index of NACA Technical Publications
Author: United States. National Advisory Committee for AeronauticsPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 274
Book Description
Handbook of Supersonic Aerodynamics
Author: George RudingerPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 452
Book Description
Author: