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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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.

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 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.

Pressure Measurements On Sharp And Blunt 5 Degreee And 15 Degree Half Angle Cones At Mach Number 3 86 And Angles Of Attack To 100 Degrees

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Author : James L. Amick
language : en
Publisher:
Release Date : 1961

Pressure Measurements On Sharp And Blunt 5 Degreee And 15 Degree Half Angle Cones At Mach Number 3 86 And Angles Of Attack To 100 Degrees written by James L. Amick 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.

Pressure Distributions On 140 160 And 180 Degree Cones At Mach Numbers From 2 30 To 4 63 And Angles Of Attack From 0 To 20 Degrees

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Author : James F. Campbell
language : en
Publisher:
Release Date : 1969

Pressure Distributions On 140 160 And 180 Degree Cones At Mach Numbers From 2 30 To 4 63 And Angles Of Attack From 0 To 20 Degrees written by James F. Campbell 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.

Experimental Determination Of Pressure Distribution Over Slender Cones At Angles Of Attack At Mach 14

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Author : Stuart E. Larsen
language : en
Publisher:
Release Date : 1965

Experimental Determination Of Pressure Distribution Over Slender Cones At Angles Of Attack At Mach 14 written by Stuart E. Larsen and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1965 with Aerodynamic load categories.

Two slender cones, L/D = 4 and L/D = 8, were tested at a nominal Mach number of 14 in air. Total pressure and temperature conditions were 1400-1600 psia and 1350-1550F., respectively. Experimental pressure data was obtained for angles of attack between 0-20 degrees and circumferential angles of 0-180 degrees. This data is presented in conjunction with Sims' and Newtonian Impact theories. (Author).

Experimental Determination Of Pressure Distribution Over Slender Cones At Angles Of Attack At Mach 14

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Author : Stuart E. Larsen
language : en
Publisher:
Release Date : 1965

Experimental Determination Of Pressure Distribution Over Slender Cones At Angles Of Attack At Mach 14 written by Stuart E. Larsen and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1965 with Aerodynamic load categories.

Two slender cones, L/D = 4 and L/D = 8, were tested at a nominal Mach number of 14 in air. Total pressure and temperature conditions were 1400-1600 psia and 1350-1550F., respectively. Experimental pressure data was obtained for angles of attack between 0-20 degrees and circumferential angles of 0-180 degrees. This data is presented in conjunction with Sims' and Newtonian Impact theories. (Author).

Shock Shapes And Pressure Distributions For Large Angle Pointed Cones In Helium At Mach Numbers Of 8 And 20

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Author : David A. Stewart
language : en
Publisher:
Release Date : 1969

Shock Shapes And Pressure Distributions For Large Angle Pointed Cones In Helium At Mach Numbers Of 8 And 20 written by David A. Stewart 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.

Experimental Pressure Distributions On A 1200 Cone At Mach Numbers From 2 96 To 4 63 And Angles Of Attack From 00 To 200

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Author : Robert L. Stallings
language : en
Publisher:
Release Date : 1969

Experimental Pressure Distributions On A 1200 Cone At Mach Numbers From 2 96 To 4 63 And Angles Of Attack From 00 To 200 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.