Flight Evaluation Of Splitter Plate Effectiveness In Reducing Base Drag At Mach Numbers From 0 65 To 0 90
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Flight Evaluation Of Splitter Plate Effectiveness In Reducing Base Drag At Mach Numbers From 0 65 To 0 90
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Author : Edwin J. Saltzman
language : en
Publisher:
Release Date : 1967
Flight Evaluation Of Splitter Plate Effectiveness In Reducing Base Drag At Mach Numbers From 0 65 To 0 90 written by Edwin J. Saltzman and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1967 with categories.
Government Reports Announcements Index
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Author :
language : en
Publisher:
Release Date : 1996
Government Reports Announcements Index written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1996 with Science categories.
International Aerospace Abstracts
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Author :
language : en
Publisher:
Release Date : 1999
International Aerospace Abstracts written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1999 with Aeronautics categories.
Influence Of Base Modifications On In Flight Base Drag In The Presence Of Jet Exhaust For Mach Numbers From 0 7 To 1 5
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Author : Sheryll Goecke Powers
language : en
Publisher:
Release Date : 1988
Influence Of Base Modifications On In Flight Base Drag In The Presence Of Jet Exhaust For Mach Numbers From 0 7 To 1 5 written by Sheryll Goecke Powers and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1988 with categories.
Flight Tests Of External Modifications Used To Reduce Blunt Base Drag
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Author :
language : en
Publisher:
Release Date : 1988
Flight Tests Of External Modifications Used To Reduce Blunt Base Drag written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1988 with categories.
Effects Of Aspect Ratio On Air Flow At A High Subsonic Mach Numbers
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Author : W. F. Lindsey
language : en
Publisher:
Release Date : 1948
Effects Of Aspect Ratio On Air Flow At A High Subsonic Mach Numbers written by W. F. Lindsey and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1948 with Air flow categories.
Schlieren photographs were used in an investigation to determine the effects of changing the aspect ratio from infinity to two on the air flow past a wing at high subsonic Mach numbers. The results indicated that the decreased effects of compressibility on drag coefficients for the finite wing are produced by a reduction in the compression shock and flow separation.
Effectiveness Of An All Movable Horizontal Tail On An Unswept Wing And Body Combination For Mach Numbers From 0 60 To 1 40
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Author : Louis S. Stivers
language : en
Publisher:
Release Date : 1959
Effectiveness Of An All Movable Horizontal Tail On An Unswept Wing And Body Combination For Mach Numbers From 0 60 To 1 40 written by Louis S. Stivers and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1959 with Mach number 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.
The Effectiveness At High Subsonic Mach Numbers Of A 20 Percent Chord Plain Trailing Edge Flap On The Naca 65 210 Airfoil Section
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Author : Louis S. Stivers
language : en
Publisher:
Release Date : 1954
The Effectiveness At High Subsonic Mach Numbers Of A 20 Percent Chord Plain Trailing Edge Flap On The Naca 65 210 Airfoil Section written by Louis S. Stivers 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.