Aerodynamic Characteristics Of Several Low Aspect Ratio Stabilizer Fins At Mach Numbers From 0 8 To 1 3
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Aerodynamic Characteristics Of Several Low Aspect Ratio Stabilizer Fins At Mach Numbers From 0 8 To 1 3
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Author : J. M. Whoric
language : en
Publisher:
Release Date : 1972
Aerodynamic Characteristics Of Several Low Aspect Ratio Stabilizer Fins At Mach Numbers From 0 8 To 1 3 written by J. M. Whoric and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1972 with Cylinders categories.
Aerodynamic Characteristics Of Several Low Aspect Ratio Stabilizer Fins At Mach Numbers From 0 8 To 1 3
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Author : J. M. Whoric
language : en
Publisher:
Release Date : 1972
Aerodynamic Characteristics Of Several Low Aspect Ratio Stabilizer Fins At Mach Numbers From 0 8 To 1 3 written by J. M. Whoric and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1972 with Cylinders categories.
Aerodynamic Characteristics Of Low Aspect Ratio Fins At Mach Numbers From 0 80 To 1 30
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Author : D.K. Smith
language : en
Publisher:
Release Date : 1971
Aerodynamic Characteristics Of Low Aspect Ratio Fins At Mach Numbers From 0 80 To 1 30 written by D.K. Smith and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1971 with Cylinders categories.
Aerodynamic Characteristics Of Low Aspect Ratio Fins At Mach Numbers From 0 80 To 1 30
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Author : D.K. Smith
language : en
Publisher:
Release Date : 1971
Aerodynamic Characteristics Of Low Aspect Ratio Fins At Mach Numbers From 0 80 To 1 30 written by D.K. Smith and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1971 with Cylinders categories.
Effect Of Fin Flare Combinations On The Aerodynamic Characteristics Of A Body At Mach Numbers 1 61 And 2 20
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Author : Clyde Hayes
language : en
Publisher:
Release Date : 1965
Effect Of Fin Flare Combinations On The Aerodynamic Characteristics Of A Body At Mach Numbers 1 61 And 2 20 written by Clyde Hayes and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1965 with Lift (Aerodynamics) categories.
The Aerodynamic Characteristics Of Wrap Around Fins At Mach Numbers Of 0 3 To 3 0
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Author : C. Wayne Dahlke
language : en
Publisher:
Release Date : 1976
The Aerodynamic Characteristics Of Wrap Around Fins At Mach Numbers Of 0 3 To 3 0 written by C. Wayne Dahlke and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1976 with Guided missiles categories.
Results of investigations into many of the geometric and flow parameters influencing the aerodynamics of wrap-around fins are presented in this report. Particular emphasis is placed on defining static and dynamic roll characteristics between Mach numbers of 0.3 to 3.0. Among the geometric parameters highlighted are fin span, aspect ratio, leading edge sweep, leading edge shape, fin opening angle, and afterbody geometry. Comparisons of static stability, dynamic stability, and drag are made between the flat and the wrap- around fin. Problems associated with measurement of wrap-around fin rolling mounts are also discussed. An overview of the wrap-around fin roll moment characteristics are presented as an aid for making estimates and establishing testing techniques. This report supercedes RD-73-17.
Aerodynamic Characteristics Of Low Aspect Ratio Wings At High Supersonic Mach Numbers
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Author : Edward F. Ulmann
language : en
Publisher:
Release Date : 1953
Aerodynamic Characteristics Of Low Aspect Ratio Wings At High Supersonic Mach Numbers written by Edward F. Ulmann 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.
A Summary Of Aerodynamic Characteristics For Wrap Around Fins From Mach 0 3 To 3 0
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Author : James A. Humphrey
language : en
Publisher:
Release Date : 1977
A Summary Of Aerodynamic Characteristics For Wrap Around Fins From Mach 0 3 To 3 0 written by James A. Humphrey and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1977 with Aerodynamics categories.
Wrap-around fin effectiveness for tube-launched missiles was investigated in a series of 6 wind tunnel tests. Wind tunnels were AEDC Propulsion Wind Tunnel, NASA/Langley Research Center Unitary Plan Wind Tunnel and McDonnell Douglas 4-foot Trisonic Wind Tunnel. Mach number range was 0.3 to 3.0. Basic model was a 2-caliber secant ogive nose with an 8-caliber cylindrical afterbody and 21 fin configurations. Variations in the coefficients are presented for changes in fin geometry including taper ratio and leading edge sweep angle, aspect ratio, exposed semi-span, and root chord length; opening angle, fully closed to 10 deg past fully open; and body step down.
New Results In Numerical And Experimental Fluid Mechanics Vi
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Author : Cameron Tropea
language : en
Publisher: Springer Science & Business Media
Release Date : 2007-10-26
New Results In Numerical And Experimental Fluid Mechanics Vi written by Cameron Tropea and has been published by Springer Science & Business Media this book supported file pdf, txt, epub, kindle and other format this book has been release on 2007-10-26 with Computers categories.
This volume features the contributions to the 15th Symposium of the STAB (German Aerospace Aerodynamics Association). Papers provide a broad overview of ongoing work in Germany, including high aspect ratio wings, low aspect ratio wings, bluff bodies, laminar flow control and transition, active flow control, hypersonic flows, aeroelasticity, aeroacoustics, mathematical fundamentals, numerical simulations, physical fundamentals, and facilities.
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.