Free Flight Investigation At Mach Numbers Between 0 5 And 1 7 Of The Zero Lift Rolling Effectiveness And Drag Of Various Surface Spoiler And Jet Controls On An 80 Delta Wing Missile
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Free Flight Investigation At Mach Numbers Between 0 5 And 1 7 Of The Zero Lift Rolling Effectiveness And Drag Of Various Surface Spoiler And Jet Controls On An 80 Delta Wing Missile
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Author : Eugene D. Schult
language : en
Publisher:
Release Date : 1960
Free Flight Investigation At Mach Numbers Between 0 5 And 1 7 Of The Zero Lift Rolling Effectiveness And Drag Of Various Surface Spoiler And Jet Controls On An 80 Delta Wing Missile written by Eugene D. Schult 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.
Nasa Technical Note
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Author :
language : en
Publisher:
Release Date : 1960
Nasa Technical Note 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.
Index Of Nasa Technical Publications
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Author : United States. National Aeronautics and Space Administration
language : en
Publisher:
Release Date : 1959
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 1959 with Aeronautics categories.
Government Reports Announcements Index
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Author :
language : en
Publisher:
Release Date : 1983
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 1983 with Science categories.
Flying Magazine
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Author :
language : en
Publisher:
Release Date : 2000-02
Flying Magazine written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2000-02 with categories.
Popular Mechanics
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Author :
language : en
Publisher:
Release Date : 1964-04
Popular Mechanics written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1964-04 with categories.
Popular Mechanics inspires, instructs and influences readers to help them master the modern world. Whether it’s practical DIY home-improvement tips, gadgets and digital technology, information on the newest cars or the latest breakthroughs in science -- PM is the ultimate guide to our high-tech lifestyle.
Free Flight Measurements Of The Zero Lift Drag Of Several Wings At Mach Numbers From 1 4 To 3 8
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Author : H. Herbert Jackson
language : en
Publisher:
Release Date : 1960
Free Flight Measurements Of The Zero Lift Drag Of Several Wings At Mach Numbers From 1 4 To 3 8 written by H. Herbert Jackson 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.
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.
Free Flight Investigation Of The Zero Lift Drag Of Several Wings At Supersonic Mach Numbers Extending To 2 6
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Author : Russell N. Hopko
language : en
Publisher:
Release Date : 1952
Free Flight Investigation Of The Zero Lift Drag Of Several Wings At Supersonic Mach Numbers Extending To 2 6 written by Russell N. Hopko 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.
Lift Drag Static Stability And Buffet Boundaries Of A Model Of The Mcdonnell F3h 1n Airplane At Mach Numbers From 0 40 To 1 27 Ted No Naca De 351
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Author : Norman L. Crabill
language : en
Publisher: BiblioGov
Release Date : 2013-06
Lift Drag Static Stability And Buffet Boundaries Of A Model Of The Mcdonnell F3h 1n Airplane At Mach Numbers From 0 40 To 1 27 Ted No Naca De 351 written by Norman L. Crabill and has been published by BiblioGov this book supported file pdf, txt, epub, kindle and other format this book has been release on 2013-06 with categories.
The National Advisory Committee for Aeronautics has conducted a flight test of a model approximating the McDonnell F3H-lN airplane configuration to determine its pitch-up and buffet boundaries, as well as the usual longitudinal stability derivatives obtainable from the pulsed- tail technique. The test was conducted by the freely flying rocket- boosted model technique developed at the Langley Laboratory; results were obtained at Mach numbers from 0.40 to 1.27 at corresponding Reynolds numbers of 2.6 x 10(exp 6) and 9.0 x 10(exp 6). The phenomena of pitch-up, buffet, and maximum lift were encountered at Mach numbers between 0.42 and 0.85. The lift-curve slope and wing-root bending-moment slope increased with increasing angle of attack, whereas the static stability decreased with angle of attack at subsonic speeds and increased at transonic speeds. There was little change in trim at low lift at transonic speeds.