A Flight Investigation To Determine The Effectiveness Of Mach Number 1 0 1 2 And 1 41 Fuselage Indentations For Reducing The Pressure Drag Of A 45 Degree Sweptback Wing Configuration At Transonic And Low Supersonic Speeds
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Index Of Nasa Technical Publications
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Author : United States. National Aeronautics and Space Administration
language : en
Publisher:
Release Date : 1960
Index Of 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 with Aeronautics categories.
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.
Index Of Naca Technical Publications
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1956
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 1956 with Aeronautics categories.
A Selected Listing Of Nasa Scientific And Technical Reports For
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Author :
language : en
Publisher:
Release Date : 1960
A Selected Listing Of Nasa Scientific And Technical Reports For 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 Aeronautics categories.
A Flight Investigation To Determine The Effectiveness Of Mach Number 1 0 1 2 And 1 41 Fuselage Indentations For Reducing The Pressure Drag Of A 45 Degree Sweptback Wing Configuration At Transonic And Low Supersonic Speeds
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Author : Willard S. Blanchard
language : en
Publisher:
Release Date : 1957
A Flight Investigation To Determine The Effectiveness Of Mach Number 1 0 1 2 And 1 41 Fuselage Indentations For Reducing The Pressure Drag Of A 45 Degree Sweptback Wing Configuration At Transonic And Low Supersonic Speeds written by Willard S. Blanchard 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.
Investigation At Mach Numbers From 0 80 To 1 43 Of Pressure And Load Distributions Over A Thin 45 Sweptback Highly Tapered Wing In Combination With Basic And Indented Bodies
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Author : Thomas L. Fischetti
language : en
Publisher:
Release Date : 1957
Investigation At Mach Numbers From 0 80 To 1 43 Of Pressure And Load Distributions Over A Thin 45 Sweptback Highly Tapered Wing In Combination With Basic And Indented Bodies written by Thomas L. Fischetti and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1957 with Aerodynamic load categories.
Pressure distributions have been obtained in the Langley 8-foot transonic tunnels over a Mach number range from 0.80 to 1.125 and at a Mach number of 1.43 for a 45 degree sweptback cambered wing having a thickened root, an aspect ratio of 4.0, and a taper ratio of 0.15. Data were obtained for the wing in the presence of a basic Sears-Haack body and a body indented symmetrically for a Mach number of 1.2.
A Flight Investigation Of The Transonic Area Rule For A 52 5 Sweptback Wind Body Configuration At Mach Numbers Between 0 8 And 1 6
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Author : Sherwood Hoffman
language : en
Publisher:
Release Date : 1954
A Flight Investigation Of The Transonic Area Rule For A 52 5 Sweptback Wind Body Configuration At Mach Numbers Between 0 8 And 1 6 written by Sherwood Hoffman and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1954 with Aerodynamics, Transonic categories.
Effects Of A Lower Surface Jet On The Lift Drag Ratio Of A 45 Sweptback Wing At A Mach Number Of 2 01
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Author : Emma Jean Landrum
language : en
Publisher:
Release Date : 1960
Effects Of A Lower Surface Jet On The Lift Drag Ratio Of A 45 Sweptback Wing At A Mach Number Of 2 01 written by Emma Jean Landrum and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960 with Mach number categories.
Flight Measurements Of Lifting Pressures For A Thin Low Aspect Ratio Wing At Subsonic Transonic And Low Supersonic Speeds
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Author : Thomas A. Byrdsong
language : en
Publisher:
Release Date : 1977
Flight Measurements Of Lifting Pressures For A Thin Low Aspect Ratio Wing At Subsonic Transonic And Low Supersonic Speeds written by Thomas A. Byrdsong and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1977 with Aerodynamic load categories.
Free Flight Investigation At Mach Numbers From 0 8 To 1 5 Of The Effect Of A Fuselage Indentation On The Zero Lift Drag Of A 52 5 Degree Sweptback Wing Body Configuration With Symmetrically Mounted Stores On The Fuselage
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Author : Sherwood Hoffman
language : en
Publisher:
Release Date : 1958
Free Flight Investigation At Mach Numbers From 0 8 To 1 5 Of The Effect Of A Fuselage Indentation On The Zero Lift Drag Of A 52 5 Degree Sweptback Wing Body Configuration With Symmetrically Mounted Stores On The Fuselage written by Sherwood Hoffman and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1958 with categories.