An Investigation At Mach Numbers 1 94 And 2 41 Of Jet Effects Upon The Longitudinal And Directional Stability Of A General Aircraft Configuration Employing Wing Tip Mounted Nacelles
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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.
Ingenier A Aeronautica Y Astron Utica
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Author :
language : es
Publisher:
Release Date : 1963
Ingenier A Aeronautica Y Astron Utica written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1963 with Aeronautics categories.
An Investigation At Mach Numbers 1 94 And 2 41 Of Jet Effects Upon The Longitudinal And Directional Stability Of A General Aircraft Configuration Employing Wing Tip Mounted Nacelles
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Author : Frank L. Clark
language : en
Publisher:
Release Date : 1958
An Investigation At Mach Numbers 1 94 And 2 41 Of Jet Effects Upon The Longitudinal And Directional Stability Of A General Aircraft Configuration Employing Wing Tip Mounted Nacelles written by Frank L. Clark and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1958 with Airplanes categories.
Aeronautical Enginnering A Cumulative Index To A Continuing Bibliography Supplement 312
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Author :
language : en
Publisher:
Release Date : 1994
Aeronautical Enginnering A Cumulative Index To A Continuing Bibliography Supplement 312 written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1994 with categories.
Jet Effects On Longitudinal Trim Of An Airplane Configuration Measured At Mach Numbers Between 1 2 And 1 8
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Author : Robert F. Peck
language : en
Publisher:
Release Date : 1955
Jet Effects On Longitudinal Trim Of An Airplane Configuration Measured At Mach Numbers Between 1 2 And 1 8 written by Robert F. Peck and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1955 with Stability of airplanes, Longitudinal categories.
Some Effects Of Aircraft Configuration On Static Longitudinal And Directional Stability Characteristics At Supersonic Mach Numbers Below 3
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Author : M. Leroy Spearman
language : en
Publisher:
Release Date : 1959
Some Effects Of Aircraft Configuration On Static Longitudinal And Directional Stability Characteristics At Supersonic Mach Numbers Below 3 written by M. Leroy Spearman and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1959 with Aerodynamics, Supersonic categories.
Exploratory Investigation At Mach Numbers From 0 40 To 0 95 Of The Effects Of Jets Blown Over A Wing
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Author : Lawrence Elwood Putnam
language : en
Publisher:
Release Date : 1973
Exploratory Investigation At Mach Numbers From 0 40 To 0 95 Of The Effects Of Jets Blown Over A Wing written by Lawrence Elwood Putnam and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1973 with Airplanes categories.
An exploratory investigation has been made at Mach numbers from 0.40 to 0.95 to determine the effects on lift, drag, and pitching moment of blowing a jet exhaust over the upper surface of a 50 deg swept leading-edge wing. Also investigated were the effects of varying the longitudinal and vertical location of the nozzle exit on the induced effects of jet blowing.
Free Flight Investigation Of Jet Effects At Low Supersonic Mach Numbers On A Fighter Type Configuration Employing A Tail Boom Assembly
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Author : Bruce G. Jackson
language : en
Publisher:
Release Date : 1957
Free Flight Investigation Of Jet Effects At Low Supersonic Mach Numbers On A Fighter Type Configuration Employing A Tail Boom Assembly written by Bruce G. Jackson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1957 with categories.
Stability Characteristics At Mach 2 20 Of A Variable Sweep Configuration Having Pylon Mounted Nacelles With Conical Inlets
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Author :
language : en
Publisher:
Release Date : 1965
Stability Characteristics At Mach 2 20 Of A Variable Sweep Configuration Having Pylon Mounted Nacelles With Conical Inlets written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1965 with categories.
Static Longitudinal Directional And Lateral Stability And Control Data From An Investigation At A Mach Number Of 6 83 Of Two Developmental X 15 Airplane Configurations
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Author :
language : en
Publisher:
Release Date : 1960
Static Longitudinal Directional And Lateral Stability And Control Data From An Investigation At A Mach Number Of 6 83 Of Two Developmental X 15 Airplane Configurations written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960 with categories.