Aerodynamic Characteristics In Pitch And Sideslip Of A 1 15 Scale Model Of The Scout Vehicle At A Mach Number Of 2 01

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Index To Nasa Technical Publications

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Author : United States. National Aeronautics and Space Administration
language : en
Publisher:
Release Date : 1960-07

Index To Nasa Technical Publications 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 1960-07 with categories.

Journal Of The Royal Aeronautical Society

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Author :
language : en
Publisher:
Release Date : 1961

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 1961 with Aeronautics categories.

Nasa Scientific And Technical Reports

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Author : United States. National Aeronautics and Space Administration Scientific and Technical Information Division
language : en
Publisher:
Release Date : 1966

Nasa Scientific And Technical Reports written by United States. National Aeronautics and Space Administration Scientific and Technical Information Division and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1966 with Aeronautics categories.

Aerodynamic Characteristics In Pitch And Sideslip Of A 1 15 Scale Model Of The Scout Vehicle At A Mach Number Of 2 01

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Author : Ross B. Robinson
language : en
Publisher:
Release Date : 1961

Aerodynamic Characteristics In Pitch And Sideslip Of A 1 15 Scale Model Of The Scout Vehicle At A Mach Number Of 2 01 written by Ross B. Robinson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Aerodynamics categories.

Bulletin Signal Tique

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Author :
language : fr
Publisher:
Release Date : 1961

Bulletin Signal Tique written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Aeronautics categories.

Aerodynamic Characteristics In Pitch And Sideslip Of A 1 15 Scale Model Of The Scout Vehicle At A Mach Number Of 2 01

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Author : Ross B. Robinson
language : en
Publisher:
Release Date : 1961

Aerodynamic Characteristics In Pitch And Sideslip Of A 1 15 Scale Model Of The Scout Vehicle At A Mach Number Of 2 01 written by Ross B. Robinson 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.

The effects of two sets of cruciform fins, of inline and indexed fin arrangements, a flare, andACCESSORIES SUCH AS ANTENNAS, LAUNCH FITTINGS, AND CONTROL TUNNELS ON THE AERODYNAMIC CHARACTERISTICS OF THE CONFIGURATION WERE MEASURED FOR COMBINED ANGLES OF ATTACK AND SIDESLIP TO ABOUT 8 DEGREES. The investigation was made in the Langley 4- by 4-foot supersonic pressure tunnel at a Reynolds number of 4 x 10 to the 6th power per foot. (Author).

Aerodynamic Loading Characteristics At Mach Numbers From 0 80 To 1 20 Of A 1 10 Scale Three Stage Scout Model

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Author : Thomas C. Kelly
language : en
Publisher:
Release Date : 1961

Aerodynamic Loading Characteristics At Mach Numbers From 0 80 To 1 20 Of A 1 10 Scale Three Stage Scout Model written by Thomas C. Kelly and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Launch vehicles (Astronautics) categories.

Aerodynamic loads results have been obtained in the Langley 8-foot transonic pressure tunnel at Mach numbers from 0.80 to 1.20 for a 1/10-scale model of the upper three stages of the Scout vehicle. Tests were conducted through an angle-of-attack range from -8° to 8° at an average test Reynolds number per foot of about 4.0 x 106. Results indicated that the peak negative pressures associated with expansion corners at the nose and transition flare exhibit sizeable variations which occur over a relatively small Mach number range. The magnitude of the variations may cause the critical local loading condition for the full-scale vehicle to occur at a Mach number considerably lower than that at which the maximum dynamic pressure occurs in flight. The addition of protuberances simulating antennas and wiring conduits had slight, localized effects. The lift carryover from the nose and transition flare on the cylindrical portions of the model generally increased with an increase in Mach number.

Investigation Of The Static Longitudinal And Lateral Stability Characteristics Of A 0 10 Scale Model Of A Three Stage Configuration Of The Scout Research Vehicle At Mach Numbers Of 2 29 2 96 3 96 And 4 65

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Author : Lloyd S. Jernell
language : en
Publisher:
Release Date : 1961

Investigation Of The Static Longitudinal And Lateral Stability Characteristics Of A 0 10 Scale Model Of A Three Stage Configuration Of The Scout Research Vehicle At Mach Numbers Of 2 29 2 96 3 96 And 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 1961 with Launch vehicles (Astronautics) categories.

Investigation Of The Aerodynamic Characteristics Of Two Preliminary Designs Of Scout Research Vehicle At Mach Numbers From 1 77 To 4 65

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Author : Robert J. Keynton
language : en
Publisher:
Release Date : 1961

Investigation Of The Aerodynamic Characteristics Of Two Preliminary Designs Of Scout Research Vehicle At Mach Numbers From 1 77 To 4 65 written by Robert J. Keynton and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Aerodynamics, Supersonic 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.