Experimental Aerodynamic Characteristics Of 120 Degree Included Angle Cone With Attached And Separated 20 Degree Included Angle Cone At Mach Numbers Of 2 36 And 2 70
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Experimental Aerodynamic Characteristics Of 120 Degree Included Angle Cone With Attached And Separated 20 Degree Included Angle Cone At Mach Numbers Of 2 36 And 2 70
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Author : UNITED STATES. NATIONAL AERONAUTICS AND SPACE ADMINISTRATION.
language : en
Publisher:
Release Date : 1966
Experimental Aerodynamic Characteristics Of 120 Degree Included Angle Cone With Attached And Separated 20 Degree Included Angle Cone At Mach Numbers Of 2 36 And 2 70 written by UNITED STATES. NATIONAL AERONAUTICS AND SPACE ADMINISTRATION. and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1966 with categories.
Experimental Aerodynamic Characteristics Of 120 Included Angle Cone With Attached And Separated 20 Included Angle Cone At Mach Numbers Of 2 36 And 2 70
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Author : Clarence A. Jr Brown
language : en
Publisher:
Release Date : 1972
Experimental Aerodynamic Characteristics Of 120 Included Angle Cone With Attached And Separated 20 Included Angle Cone At Mach Numbers Of 2 36 And 2 70 written by Clarence A. Jr Brown and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1972 with categories.
Experimental Pressure Distributions On A 120 Cone At Mach Numbers From 2 96 To 4 63 And Angles Of Attack From 0 To 20
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Author : Robert L. Stallings
language : en
Publisher:
Release Date : 1969
Experimental Pressure Distributions On A 120 Cone At Mach Numbers From 2 96 To 4 63 And Angles Of Attack From 0 To 20 written by Robert L. Stallings and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1969 with Aerodynamic load categories.
Aerodynamic Investigation Of Sharp Cone Cylinder Spikes On 120 Blunted Cones At Mach Numbers Of 3 00 4 50 And 6 00
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Author : Robert J. McGhee
language : en
Publisher:
Release Date : 1969
Aerodynamic Investigation Of Sharp Cone Cylinder Spikes On 120 Blunted Cones At Mach Numbers Of 3 00 4 50 And 6 00 written by Robert J. McGhee and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1969 with Blunt bodies categories.
Experimental Pressure Distributions On A 120 Degree Cone At Mach Numbers From 2 96 To 4 63 And Angles Of Attack From 0 Degree To 20 Degree
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Author : Robert L. Stallings
language : en
Publisher:
Release Date : 1976
Experimental Pressure Distributions On A 120 Degree Cone At Mach Numbers From 2 96 To 4 63 And Angles Of Attack From 0 Degree To 20 Degree written by Robert L. Stallings and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1976 with categories.
Experimental Pressure Distributions On A 120 Degrees Cone At Mach Numbers From 2 96 To 4 63 And Angles Of Attack From 0 Degrees To 20 Degrees
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Author : Robert L. Jr Stallings
language : en
Publisher:
Release Date : 1969
Experimental Pressure Distributions On A 120 Degrees Cone At Mach Numbers From 2 96 To 4 63 And Angles Of Attack From 0 Degrees To 20 Degrees written by Robert L. Jr Stallings and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1969 with categories.
Measurements Of Pressure And Local Heat Transfer On A 20 Degree Cone At Angles Of Attack Up To 20 Degrees For A Mach Number Of 4 95
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Author : Jerome D. Julius
language : en
Publisher:
Release Date : 1959
Measurements Of Pressure And Local Heat Transfer On A 20 Degree Cone At Angles Of Attack Up To 20 Degrees For A Mach Number Of 4 95 written by Jerome D. Julius and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1959 with categories.
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).
Experimental Wake Survey Behind A 120 Deg Included Angle Cone At Angles Of Attack Of 0 Deg And 5 Deg Mach Numbers From 1 60 To 3 95 And Longitudinal Stations Varying From 1 0 To 8 39 Body Diameters
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Author :
language : en
Publisher:
Release Date : 1971
Experimental Wake Survey Behind A 120 Deg Included Angle Cone At Angles Of Attack Of 0 Deg And 5 Deg Mach Numbers From 1 60 To 3 95 And Longitudinal Stations Varying From 1 0 To 8 39 Body Diameters written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1971 with categories.
Static Aerodynamic Characteristics Of Short Blunt Cones With Various Nose And Base Cone Angles At Mach Numbers From 0 6 To 5 5 And Angles Of Attack To 180 Degrees
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Author : Stuart L. Treon
language : en
Publisher:
Release Date : 1961
Static Aerodynamic Characteristics Of Short Blunt Cones With Various Nose And Base Cone Angles At Mach Numbers From 0 6 To 5 5 And Angles Of Attack To 180 Degrees written by Stuart L. Treon and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Fluid mechanics categories.