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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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
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Release Date : 1962

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Applied Mechanics Reviews

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Author :
language : en
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Release Date : 1962

Applied Mechanics Reviews 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 Mechanics, Applied categories.

The Journal Of The Royal Aeronautical Society

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Author :
language : en
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Release Date : 1962

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Scientific And Technical Aerospace Reports

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Author :
language : en
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Release Date : 1980

Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1980 with Aeronautics categories.

Technical Abstract Bulletin

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Author :
language : en
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Release Date : 1980

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 1980 with Science categories.

Nasa Scientific And Technical Publications

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Author :
language : en
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Release Date : 1987

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Bulletin Signal Tique

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Author :
language : fr
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Release Date : 1963

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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.

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.