Author: C. H. Wilts
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 362
Book Description
Investigation of the Drag of Various Axially Symmetric Nose Shapes of Fineness Ratio 3 for Mach Numbers from 1.24 to 7.4
Author: C. H. Wilts
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 362
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 362
Book Description
Investigation of the Drag of Various Axially Symmetric Nose Shapes of Fineness Ratio 3 for Mach Numbers from 1.24 to 3.67
Author: Edward W. Perkins
Publisher:
ISBN:
Category :
Languages : en
Pages : 50
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 50
Book Description
Investigation of the Drag of Various Axially Symmetric Nose Shapes of Fineness Ratio 3 for Mach Numbers from 1.24 to 7.4
Author: Edward W. Perkins
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 17
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 17
Book Description
Investigation of the Drag of Various Axially Symmetric Nose Shapes of Fineness Ratio 3 for Mach Numbers Form 1.24 to 7.4
Author: Edward W. Perkins
Publisher:
ISBN:
Category :
Languages : en
Pages : 17
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 17
Book Description
Investigation of the Drag of Various Axially Symmetric Noise Shapes of Fineness Ratio 3 for Mach Numbers from 1.24 to 7.4
Author: Edward W. Perkins
Publisher:
ISBN:
Category :
Languages : en
Pages : 17
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 17
Book Description
Free-flight Measurements of the Transonic Drag Characteristics of Low-fineness-ratio Cylinders Including Stabilizing Plates and Flares and Varying Nose Bluntness
Author: Joseph H. Judd
Publisher:
ISBN:
Category : Drag (Aerodynamics)
Languages : en
Pages : 20
Book Description
Publisher:
ISBN:
Category : Drag (Aerodynamics)
Languages : en
Pages : 20
Book Description
Investigation of the Drag of Blunt-nosed Bodies of Revolution in Free Flight at Mach Numbers from 0.6 to 2.3
Author: Harvey A. Wallskog
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 32
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 32
Book Description
Drag Measurements at Transonic Speeds of Two Bodies of Fineness Ratio 9 with Different Locations of Maximum Body Diameter
Author: Jim Rogers Thompson
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 26
Book Description
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 26
Book Description
The Effect of Bluntness on the Drag of Spherical-tipped Truncated Cones of Fineness Ratio 3 at Mach Numbers 1.2 to 7.4
Author: Simon C. Sommer
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 26
Book Description
Abstract: The drag of spherically blunted conical models of fineness ratio 3 was investigated in the Ames super-sonic free-flight wind tunnel at Mach numbers from 1.2 to 7.4 in the Reynolds number range from 1.0 x 106 to 7.5 x 106. The models tested had bluntness ratios of nose diameter to base diameter from 0 to 0.50. The use of small amounts of bluntness for minimizing drag and the drag penalties associated with large bluntnesses are discussed.
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 26
Book Description
Abstract: The drag of spherically blunted conical models of fineness ratio 3 was investigated in the Ames super-sonic free-flight wind tunnel at Mach numbers from 1.2 to 7.4 in the Reynolds number range from 1.0 x 106 to 7.5 x 106. The models tested had bluntness ratios of nose diameter to base diameter from 0 to 0.50. The use of small amounts of bluntness for minimizing drag and the drag penalties associated with large bluntnesses are discussed.
Summary of Static Stability and Drag Characteristics of Axisymmetric Low-drag Shapes for the Subsonic to Hypersonic Mach Number Range
Author: Amado A. Trujillo
Publisher:
ISBN:
Category : Drag (Aerodynamics)
Languages : en
Pages : 44
Book Description
Publisher:
ISBN:
Category : Drag (Aerodynamics)
Languages : en
Pages : 44
Book Description