Basic Pressure Measurements At A Mach Number Of 1 43 On A Thin 45 Deg Sweptback Highly Tapered Wing With Systematic Spanwise Twist Variations

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Basic Pressure Measurements At A Mach Number Of 1 43 On A Thing 45 Degree Sweptback Highly Tapered Wing With Systematic Spanwise Twist Variations

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Author : John P. Jr Mugler
language : en
Publisher:
Release Date : 1960

Basic Pressure Measurements At A Mach Number Of 1 43 On A Thing 45 Degree Sweptback Highly Tapered Wing With Systematic Spanwise Twist Variations written by John P. Jr Mugler and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960 with Wall pressure (Aerodynamics) categories.

Pressure distributions are presented on four wings: an untwisted wing to serve as a reference, and wings with linear, quadratic, and cubic twist variations along the span. All the twisted wings had 0 degrees twist at the 10-percent-semispan station and 6 degrees twist at he tip. The tests were made at a Mach number of 1.43 and covered an angle-of-attack range from -4 degrees to 20 degrees. The average Reynolds number based on the wing mean aerodynamic chord was 2.9 X 10(6) during tests at a stagnation pressure of 1.0 atmosphere and 1.5 X 10(6) during tests at a stagnation pressure of 0.5 atmosphere.

The Journal Of The Royal Aeronautical Society

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Author :
language : en
Publisher:
Release Date : 1961

The Journal Of The Royal Aeronautical Society written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Aeronautics categories.

Journal Of The Royal Aeronautical Society

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Author :
language : en
Publisher:
Release Date : 1961

Journal Of The Royal Aeronautical Society written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Aeronautics categories.

Publications Announcements

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Author : United States. National Aeronautics and Space Administration
language : en
Publisher:
Release Date : 1958

Publications Announcements 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 1958 with Aeronautics categories.

Basic Pressure Measurements At A Mach Number Of 1 43 On A Thin 45 Deg Sweptback Highly Tapered Wing With Systematic Spanwise Twist Variations

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Author :
language : en
Publisher:
Release Date : 1960

Basic Pressure Measurements At A Mach Number Of 1 43 On A Thin 45 Deg Sweptback Highly Tapered Wing With Systematic Spanwise Twist Variations 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.

Pressure distributions are presented on four wings: an untwisted wing to serve as a reference, and wings with linear, quadratic and cubic twist variations along the span. All the twisted wings had 0deg twist at the 10-percent-semispan station and 6deg twist at the tip. The tests were made at a Mach number of 1.43 and covered an angle-of-attack range from -4deg to 20deg. The average Reynolds number based on the wing mean aerodynamic chord was 2.9 x 10(exp 6) during tests at a stagnation pressure of 1.0 atmosphere and 1.5 x 10(exp 6) during tests at a stagnation pressure of 0.5 atmosphere.

Basic Pressure Measurements At A Mach Number Of 1 43 On A Thin 45 Sweptback Highly Tapered Wing With Systematic Spanwise Twist Variations

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Author : John P. Mugler
language : en
Publisher:
Release Date : 1960

Basic Pressure Measurements At A Mach Number Of 1 43 On A Thin 45 Sweptback Highly Tapered Wing With Systematic Spanwise Twist Variations written by John P. Mugler 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.

Basic Pressure Measurements At Transonic Speeds On Thin 45 Sweptback Highly Tapered Wing With Systematic Spanwise Twist Variations Wing With Cubic Spanwise Twist Variation With List Of References

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Author :
language : en
Publisher:
Release Date : 1959

Basic Pressure Measurements At Transonic Speeds On Thin 45 Sweptback Highly Tapered Wing With Systematic Spanwise Twist Variations Wing With Cubic Spanwise Twist Variation With List Of References written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1959 with Airplanes 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.

Investigation At Mach Numbers From 0 80 To 1 43 Of Pressure And Load Distributions Over A Thin 45 Degree 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 Degree 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 Comparison At Mach Numbers Up To 0 92 Of The Calculated And Experimental Downwash And Wake Characteristics At Various Horizonatl Tail Heights Behind A Wing With 45 Degrees Of Sweepback

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Author : Jack D. Stephenson
language : en
Publisher:
Release Date : 1955

A Comparison At Mach Numbers Up To 0 92 Of The Calculated And Experimental Downwash And Wake Characteristics At Various Horizonatl Tail Heights Behind A Wing With 45 Degrees Of Sweepback written by Jack D. Stephenson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1955 with Aeronautics categories.