Related Books
Language: en
Pages: 0
Pages: 0
Language: en
Pages: 100
Pages: 100
Type: BOOK - Published: 1932 - Publisher:
Language: en
Pages: 852
Pages: 852
Type: BOOK - Published: 1952 - Publisher:
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 t
Language: en
Pages: 50
Pages: 50
Type: BOOK - Published: 1988 - Publisher:
Language: en
Pages: 28
Pages: 28
Type: BOOK - Published: 1972 - Publisher:
The experimental and analytical investigation included solid blades with five different trailing-edge thicknesses and four different trailing-edge geometries. O