Aerodynamic Characteristics Of Towed Spheres Conical Rings And Cones Used As Decelerators At Mach Numbers From 1 57 To 4 65

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Journal Of The British Interplanetary Society

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Author : British Interplanetary Society
language : en
Publisher:
Release Date : 1934

Journal Of The British Interplanetary Society written by British Interplanetary Society and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1934 with Rockets (Aeronautics) categories.

Aerodynamic Characteristics Of Towed Spheres Conical Rings And Cones Used As Decelerators At Mach Numbers From 1 57 To 4 65

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Author : Nickolai Charczenko
language : en
Publisher:
Release Date : 1963

Aerodynamic Characteristics Of Towed Spheres Conical Rings And Cones Used As Decelerators At Mach Numbers From 1 57 To 4 65 written by Nickolai Charczenko and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1963 with Cone categories.

An investigation was made to determine the drag and stability characteristics of the various decelerators when towed in the wake of several space-vehicle configurations at Mach numbers from 1.57 to 4.65. The following parameters were varied: Reynolds number, trailling distance, ratio of deceleration base diameter to space-vehicle base diameter, cone angle, and size of disk added to the base of a cone.

Aerodynamic Characteristics Of Towed Cones Used As Decelerators At Mach Numbers Rom 1 57 To 4 65

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Author : Nickolai Charczenko
language : en
Publisher:
Release Date : 1962

Aerodynamic Characteristics Of Towed Cones Used As Decelerators At Mach Numbers Rom 1 57 To 4 65 written by Nickolai Charczenko and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1962 with Aerodynamics categories.

Towed and sting-supported cones were tested in the wake of various payloads at supersonic speeds to determine their drag and stability characteristics. The investigation extended over a Mach number range from 1.57 to 4.65 and included such variables as Reynolds number, cone angle, ratio of cone base diameter to payload base diameter, and trailing distance. Cones towed in the wake of a symmetrical payload at supersonic speeds, in general, had good drag and stability characteristics if towed in the supersonic flow region. A cone with an included angle between 80 and 90 degrees gave 2 maximum drag while still maintaining stability. In order to minimize wake effects, the ratio of cone base diameter to payload base diameter should be at least one and preferably around three. A trailing distance of three times the payload base diameter, in most cases, is of sufficient length to avoid low drag and instability of the decelerator. (Author).

Aerondynamic Characteristics Of Towed Spheres Conical Rings And Cones Used As Deceleratiors At Mach Numbers From 1 57 To 4 65

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Author : Nickolai Charczenko
language : en
Publisher:
Release Date : 1963

Aerondynamic Characteristics Of Towed Spheres Conical Rings And Cones Used As Deceleratiors At Mach Numbers From 1 57 To 4 65 written by Nickolai Charczenko and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1963 with categories.

Aerodynamic Characteristics Of Towed Cones Used As Decelerators At Mach Numbers From 1 57 To 4 65

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Author : Nickolai Charczenko
language : en
Publisher:
Release Date : 1961

Aerodynamic Characteristics Of Towed Cones Used As Decelerators At Mach Numbers From 1 57 To 4 65 written by Nickolai Charczenko and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with categories.

Towed and sting-supported cones were tested in the wake of various payloads at supersonic speeds to determine their drag and stability characteristics. The investigation extended over a Mach number range from 1.57 to 4.65 and included such variables as Reynolds number, cone angle, ratio of cone base diameter to payload base diameter, and trailing distance. Cones towed in the wake of a symmetrical payload at supersonic speeds, in general, had good drag and stability characteristics if towed in the supersonic flow region. A cone with an included angle between 80 and 90 degrees gave 2 maximum drag while still maintaining stability. In order to minimize wake effects, the ratio of cone base diameter to payload base diameter should be at least one and preferably around three. A trailing distance of three times the payload base diameter, in most cases, is of sufficient length to avoid low drag and instability of the decelerator. (Author).

Aerodynamic Characteristics Of Spherically Blunted Cones At Mach Numbers From 0 5 To 5 0

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Author : Robert V. Owens
language : en
Publisher:
Release Date : 1965

Aerodynamic Characteristics Of Spherically Blunted Cones At Mach Numbers From 0 5 To 5 0 written by Robert V. Owens and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1965 with Aerodynamics categories.

Sphere Cone Cone Surface Pressure Distribution At Mach Numbers Of 5 6 8 And 10

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Author : R. R. Eaton
language : en
Publisher:
Release Date : 1968

Sphere Cone Cone Surface Pressure Distribution At Mach Numbers Of 5 6 8 And 10 written by R. R. Eaton and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1968 with Aerodynamic load categories.

Longitudinal Aerodynamic Characteristics Of Blunted Cones At Mach Numbers Of 3 5 4 2 And 6 0

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Author : J. Wayne Keyes
language : en
Publisher:
Release Date : 1964

Longitudinal Aerodynamic Characteristics Of Blunted Cones At Mach Numbers Of 3 5 4 2 And 6 0 written by J. Wayne Keyes and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1964 with Atmosphere, Upper categories.

Static Aerodynamic Characteristics Of A Short Blunt 10 Degree Semivertex Angle Cone At A Mach Number Of 15 In Helium

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Author : Melvin J. Fohrman
language : en
Publisher:
Release Date : 1963

Static Aerodynamic Characteristics Of A Short Blunt 10 Degree Semivertex Angle Cone At A Mach Number Of 15 In Helium written by Melvin J. Fohrman and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1963 with Aerodynamics categories.

Aerodynamic Characteristics For Cone Cylinder Frustum Cylinder Configurations At Mach Numbers From 0 7 T0 1 96

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Author : J.F. Thompson
language : en
Publisher:
Release Date : 1967

Aerodynamic Characteristics For Cone Cylinder Frustum Cylinder Configurations At Mach Numbers From 0 7 T0 1 96 written by J.F. Thompson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1967 with categories.