Longitudinal Stability Control Effectiveness And Drag Characteristics At Transonic Speeds Of A Rocket Propelled Model Of An Airplane Configuration Having An Unswept Tapered Wing Of Aspect Ratio 3 0 And Naca 65a004 5 Airfoil Sections
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Index Of Naca Technical Publications
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1957
Index Of Naca Technical Publications written by United States. National Advisory Committee for Aeronautics and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1957 with Aeronautics categories.
Research Abstracts And Reclassification Notice
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1956
Research Abstracts And Reclassification Notice written by United States. National Advisory Committee for Aeronautics and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1956 with Aeronautics categories.
Longitudinal Stability Control Effectiveness And Drag Characteristics At Transonic Speeds Of A Rocket Propelled Model Of An Airplane Configuration Having An Unswept Tapered Wing Of Aspect Ratio 3 0 And Naca 65a004 5 Airfoil Sections
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Author : John C. Jr McFall
language : en
Publisher:
Release Date : 1953
Longitudinal Stability Control Effectiveness And Drag Characteristics At Transonic Speeds Of A Rocket Propelled Model Of An Airplane Configuration Having An Unswept Tapered Wing Of Aspect Ratio 3 0 And Naca 65a004 5 Airfoil Sections written by John C. Jr McFall and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1953 with categories.
Longitudinal Stability Characteristics At Transonic Speeds Of A Rocket Propelled Model Of An Airplane Configuration Having A 45 Degree Swept Wing Of Aspect Ratio 6 0
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Author : John C. Jr McFall
language : en
Publisher:
Release Date : 1954
Longitudinal Stability Characteristics At Transonic Speeds Of A Rocket Propelled Model Of An Airplane Configuration Having A 45 Degree Swept Wing Of Aspect Ratio 6 0 written by John C. Jr McFall and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1954 with categories.
Longitudinal Stability And Drag Characteristics At Mach Numbers From 0 75 To 1 5 Of An Airplane Configuration Having A 60 Degrees Swept Wing Of Aspect Ratio 2 24 As Obtained From Rocket Propelled Model
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Author : A. James Vitale
language : en
Publisher:
Release Date : 1952
Longitudinal Stability And Drag Characteristics At Mach Numbers From 0 75 To 1 5 Of An Airplane Configuration Having A 60 Degrees Swept Wing Of Aspect Ratio 2 24 As Obtained From Rocket Propelled Model written by A. James Vitale and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1952 with categories.
Longitudinal Stability Trim And Drag Characteristics Of A Rocket Propelled Model Of An Airplane Configuration Having A 45 Degree Sweptback Wing And An Unswept Horizontal Tail
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Author : James H. Parks
language : en
Publisher:
Release Date : 1952
Longitudinal Stability Trim And Drag Characteristics Of A Rocket Propelled Model Of An Airplane Configuration Having A 45 Degree Sweptback Wing And An Unswept Horizontal Tail written by James H. Parks and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1952 with categories.
Longitudinal Stability And Control Characteristics At Transonic Speeds Of A Semispan Airplane Model Having A 45 Degrees Sweptback Wing And Tail As Obtained By The Transonic Bump Method
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Author : M. Leroy Spearman
language : en
Publisher:
Release Date : 1948
Longitudinal Stability And Control Characteristics At Transonic Speeds Of A Semispan Airplane Model Having A 45 Degrees Sweptback Wing And Tail As Obtained By The Transonic Bump Method 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 1948 with categories.
Stability And Control Characteristics At Transonic Speeds Of Two Variable Sweep Airplane Configurations Differing In Wing Pivot Locations
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Author : Ralph P. Bielat
language : en
Publisher:
Release Date : 1961
Stability And Control Characteristics At Transonic Speeds Of Two Variable Sweep Airplane Configurations Differing In Wing Pivot Locations written by Ralph P. Bielat 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.
Lateral Stability Characteristics At Low Lift Between Mach Numbers Of 0 85 And 1 15 Of A Rocket Propelled Model Of A Supersonic Airplane Configuration Having A Tapered Wing With Circular Arc Sections And 40 Degree Sweepback
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Author : Charles T. D'Aiutolo
language : en
Publisher:
Release Date : 1955
Lateral Stability Characteristics At Low Lift Between Mach Numbers Of 0 85 And 1 15 Of A Rocket Propelled Model Of A Supersonic Airplane Configuration Having A Tapered Wing With Circular Arc Sections And 40 Degree Sweepback written by Charles T. D'Aiutolo and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1955 with categories.
Comparison Of Low Lift Drag At Mach Numbers From 0 74 To 1 37 Of Rocket Boosted Models Having Externally Braced Wings And Cantilever Wings
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Author : Waldo L. Dickens
language : en
Publisher:
Release Date : 1957
Comparison Of Low Lift Drag At Mach Numbers From 0 74 To 1 37 Of Rocket Boosted Models Having Externally Braced Wings And Cantilever Wings written by Waldo L. Dickens and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1957 with Aerofoils categories.
An investigation has been conducted to determine whether the low-lift drag of a rocket-model airplane-like configuration could be reduced at transonic and low supersonic Mach numbers by reducing the wing thickness while external braces were used to provide the necessary bending strength. The investigation consisted of flight training two rocket models having aspect ratio 3.04, unswept braced tapered wings mounted on fuselages with the same fineness ratios and cross-sectional area distributions. Data collected from the flight test of a model having a thicker cantilever wing of the same plan form were compared with data collected in this investigation.