Effect Of Shape Changes On The Aerodynamic Characteristics Of A Twisted And Cambered Arrow Wing At Mach Number 2 03
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Effect Of Shape Changes On The Aerodynamic Characteristics Of A Twisted And Cambered Arrow Wing At Mach Number 2 03
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Author : Emma Jean Landrum
language : en
Publisher:
Release Date : 1968
Effect Of Shape Changes On The Aerodynamic Characteristics Of A Twisted And Cambered Arrow Wing At Mach Number 2 03 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 1968 with Aerodynamics, Supersonic categories.
Nasa Technical Note
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Author :
language : en
Publisher:
Release Date : 1974
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 1974 with categories.
Nasa Technical Paper
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Author :
language : en
Publisher:
Release Date : 1992
Nasa Technical Paper written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1992 with Science categories.
Nasa Scientific And Technical Reports
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Author : United States. National Aeronautics and Space Administration Scientific and Technical Information Division
language : en
Publisher:
Release Date : 1968
Nasa Scientific And Technical Reports written by United States. National Aeronautics and Space Administration Scientific and Technical Information Division and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1968 with Aeronautics categories.
A Selected Listing Of Nasa Scientific And Technical Reports
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Author : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
language : en
Publisher:
Release Date : 1969
A Selected Listing Of Nasa Scientific And Technical Reports written by United States. National Aeronautics and Space Administration. Scientific and Technical Information Division and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1969 with Aeronautics categories.
The Aeronautical Journal
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Author :
language : en
Publisher:
Release Date : 1969
The Aeronautical Journal written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1969 with Aeronautics categories.
Effects Of Leading Edge Sweep Angle And Design Lift Coefficient On Performance Of A Modified Arrow Wing At A Design Mach Number Of 2 6
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Author : Robert J. Mack
language : en
Publisher:
Release Date : 1974
Effects Of Leading Edge Sweep Angle And Design Lift Coefficient On Performance Of A Modified Arrow Wing At A Design Mach Number Of 2 6 written by Robert J. Mack and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1974 with Aerodynamics, Supersonic categories.
Wing models were tested in the high-speed section of the Langley Unitary Plan wind tunnel to study the effects of the leading-edge sweep angle and the design lift coefficient on aerodynamic performance and efficiency. The models had leading-edge sweep angles of 69.44 deg, 72.65 deg, and 75.96 deg which correspond to values of the design Mach-number-sweep-angle parameter (beta cotangent A) sub DES of 0.6, 0.75, and 0.9, respectively. For each sweep angle, camber surfaces having design lift coefficients of 0,0.08, and 0.12 at a design Mach number of 2.6 were generated. The wind-tunnel tests were conducted at Mach numbers of 2.3, 2.6, and 2.96 with a stagnation temperature of 338.7 K (150 F) and a Reynolds number per meter of 9.843 times 10 to the 6th power. The results of the tests showed that only a moderate sweeping of the wing leading edge aft of the Mach line along with a small-to-moderate amount of camber and twist was needed to significantly improve the zero-lift (flat camber surface) wing performance and efficiency.
Survey And Analysis Of Research On Supersonic Drag Due To Lift Minimization With Recommendations For Wing Design
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Author : Harry W. Carlson
language : en
Publisher:
Release Date : 1992
Survey And Analysis Of Research On Supersonic Drag Due To Lift Minimization With Recommendations For Wing Design written by Harry W. Carlson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1992 with Aerodynamics, Supersonic categories.
Scientific And Technical Aerospace Reports
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Author :
language : en
Publisher:
Release Date : 1976
Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1976 with Aeronautics categories.
Aerodynamic Characteristics At Mach Number 2 01 Of An Airplane Configuration Having A Cambered And Twisted Arrow Wing Designed For A Mach Number Of 3 0
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Author : Odell A. Morris
language : en
Publisher:
Release Date : 1959
Aerodynamic Characteristics At Mach Number 2 01 Of An Airplane Configuration Having A Cambered And Twisted Arrow Wing Designed For A Mach Number Of 3 0 written by Odell A. Morris and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1959 with Aerodynamic load categories.