Static Aerodynamic Characteristics Of A Two Stage And A Three Stage Rocket Vehicle At Mach Numbers From 1 47 To 4 63

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Static Aerodynamic Characteristics Of A Two Stage And A Three Stage Rocket Vehicle At Mach Numbers From 1 47 To 4 63

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Author : Clarence A. Brown
language : en
Publisher:
Release Date : 1962

Static Aerodynamic Characteristics Of A Two Stage And A Three Stage Rocket Vehicle At Mach Numbers From 1 47 To 4 63 written by Clarence A. Brown and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1962 with Space vehicles categories.

Static Aerodynamic Characteristics Of Three Rocket Vehicle Configurations At Mach Numbers From 1 80 To 4 63 Including Some Effects Of Fin Size Fin Cant And Auxiliary Rocket Motors

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Author : Dennis E. Fuller
language : en
Publisher:
Release Date : 1963

Static Aerodynamic Characteristics Of Three Rocket Vehicle Configurations At Mach Numbers From 1 80 To 4 63 Including Some Effects Of Fin Size Fin Cant And Auxiliary Rocket Motors written by Dennis E. Fuller 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, Supersonic categories.

Static Aerodynamic Characteristics Of A Two Stage And A Three Stage Rocket Vehicle At Mach Numbers From 1 47 To 4 63

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Author : CLARENCE A. JR. BROWN
language : en
Publisher:
Release Date : 1962

Static Aerodynamic Characteristics Of A Two Stage And A Three Stage Rocket Vehicle At Mach Numbers From 1 47 To 4 63 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 1962 with categories.

An investigation was conducted in the Langley Unitary Plan wind tunnel to determine the effects of fin cant and size on the static aerodynamic characteristics of a 0.081-scale model of a three-stage and a two-stage Trailblazer II configuration. Tests were performed at Mach numbers from 1.47 to 4.63 and at a Reynolds number per foot of 3.0 x 10 to the 6th power. he angleof-attack range varied from approximately -5 to 5 degrees and angle of sideslip varied from approximately -4 to 4 degrees. All first-stage fins tested gave adequate static stability when the center-of-gravity travel of the flight model was taken into account. The presence of the auxiliary rocket motors in the lateral plane decreased the effectiveness of the fins in the pitch plane at the lower Mach number and increased the fin effectiveness at the higher Mach numbers. Removal of the auxiliary rocket motors from the first stage of the two-stage configuration reduced the axial force about 25% at the low Mach numbers and about 15% at the high Mach numbers. (Author).

Static Aerodynamic Characteristics Of A Three Stage Rocket Vehicle Having Various Fin Configurations At Low Subsonic Mach Numbers And Angles Of Attack Up To 28

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Author : Clarence A. Brown
language : en
Publisher:
Release Date : 1963

Static Aerodynamic Characteristics Of A Three Stage Rocket Vehicle Having Various Fin Configurations At Low Subsonic Mach Numbers And Angles Of Attack Up To 28 written by Clarence A. Brown and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1963 with Angle of attack (Aerodynamics) categories.

Aerodynamic Characteristics In Pitch Of A 1 7 Scale Model Of A Two And Three Stage Rocket Configuration At Mach Numbers Of 0 4 To 4 63

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Author : William F. Hinson
language : en
Publisher:
Release Date : 1969

Aerodynamic Characteristics In Pitch Of A 1 7 Scale Model Of A Two And Three Stage Rocket Configuration At Mach Numbers Of 0 4 To 4 63 written by William F. Hinson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1969 with Pitching (Aerodynamics) categories.

Aerodynamic characteristics in pitch of scale model of two and three stage rocket configuration at Mach numbers of 0.4 to 4.63.

Static Stability And Separation Characteristics Of A Two Stage Rocket Configuration At Mach Numbers From 1 57 To 4 50

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Author : Kenneth L. Turner
language : en
Publisher:
Release Date : 1960

Static Stability And Separation Characteristics Of A Two Stage Rocket Configuration At Mach Numbers From 1 57 To 4 50 written by Kenneth L. Turner and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960 with Aerodynamics, Supersonic categories.

Static Aerodynamic Characteristics Of A Three Stage Rocket Vehicle Having Various Fin Configurations At Low Subsonic Mach Numbers And Angles Of Attack Up To 28 Degrees

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Author : Clarence A. Jr Brown
language : en
Publisher:
Release Date : 1963

Static Aerodynamic Characteristics Of A Three Stage Rocket Vehicle Having Various Fin Configurations At Low Subsonic Mach Numbers And Angles Of Attack Up To 28 Degrees 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 1963 with categories.

Aerodynamic Loading Characteristics Of A 1 10 Scale Model Of The Three Stage Scout Vehicle At Mach Numbers 1 57 To 4 65

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Author : Lloyd S. Jernell
language : en
Publisher:
Release Date : 1963

Aerodynamic Loading Characteristics Of A 1 10 Scale Model Of The Three Stage Scout Vehicle At Mach Numbers 1 57 To 4 65 written by Lloyd S. Jernell and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1963 with Aerodynamic load categories.

Technical Abstract Bulletin

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Author :
language : en
Publisher:
Release Date :

Technical Abstract Bulletin written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on with Science categories.

Journal Of The Royal Aeronautical Society

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Author :
language : en
Publisher:
Release Date : 1962

Journal Of The Royal Aeronautical Society written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1962 with Aeronautics categories.