Investigation At Transonic Speeds Of The Loading Over A 45 Degree Sweptback Wing Having An Aspect Ratio Of 3 A Taper Ratio Of 0 2 And Naca 65a004 Airfoil Sections
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Investigation At Transonic Speeds Of The Loading Over A 45 Degree Sweptback Wing Having An Aspect Ratio Of 3 A Taper Ratio Of 0 2 And Naca 65a004 Airfoil Sections
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Author : Jack F. Runckel
language : en
Publisher:
Release Date : 1956
Investigation At Transonic Speeds Of The Loading Over A 45 Degree Sweptback Wing Having An Aspect Ratio Of 3 A Taper Ratio Of 0 2 And Naca 65a004 Airfoil Sections written by Jack F. Runckel and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1956 with Aerodynamic load categories.
An investigation at transonic speeds of the loading over a 45 degree sweptback wing having an aspect ratio of 3, a taper ratio of 0.2, and NACA 65A004 airfoil sections has been conducted in the Langley16-foot transonic tunnel. Pressure measurements on the wing-body combination were obtained at angles of attack from 0 to 26 degrees at Mach numbers from 0.80 to 0.98 and from 0 to about 12 degrees at Mach numbers from 1.00 to 1.05. Reynolds number, based on the wing mean aerodynamic chord, varied from 7,000,000 to 8,500,000 over the test Mach number range.
Technical Abstract Bulletin
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Author : Defense Documentation Center (U.S.)
language : en
Publisher:
Release Date : 1961-07
Technical Abstract Bulletin written by Defense Documentation Center (U.S.) and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961-07 with Technology categories.
Transonic Wind Tunnel Investigation Of Aerodynamic Loading Characteristics Of A 2 Percent Thick Trapezoidal Wing In Combination With Basic And Indented Bodies
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Author : Thomas C. Kelly
language : en
Publisher:
Release Date : 1957
Transonic Wind Tunnel Investigation Of Aerodynamic Loading Characteristics Of A 2 Percent Thick Trapezoidal Wing In Combination With Basic And Indented Bodies written by Thomas C. Kelly 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 data have been obtained in the Langley 8-foot transonic tunnel at Mach numbers from 0.80 to 1.115 and angles of attack from 0 to 20 degrees for wing-body configurations employing a thin trapezoidal wing in combination with basic and indented bodies. The wing had 26.6 degrees sweepback of the quarter-chord line, an aspect ratio of 2.61, a taper ratio of 0.211, and 2-percent-thick symmetrical circular-arc airfoil sections parallel to the plane of symmetry. Results are also presented for the basic body alone. Reynolds numbers for the tests were on the order of 2,600,000, based on the wing mean aerodynamic chord.
Scientific And Technical Aerospace Reports
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Author :
language : en
Publisher:
Release Date : 1963
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 1963 with Aeronautics categories.
Bibliography Of Scientific And Industrial Reports
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Author :
language : en
Publisher:
Release Date : 1961
Bibliography Of Scientific And Industrial 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 1961 with Research categories.
Technical Report
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Author : Aeronautical Research Council (Great Britain)
language : en
Publisher:
Release Date : 1971
Technical Report written by Aeronautical Research Council (Great Britain) and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1971 with Aeronautics categories.
Includes its Reports, which are also issued separately.
Investigation At Transonic Speeds Of Loading Over A 30 Deg Sweptback Wing Of Aspect Ratio 3 Taper Ratio 0 2 And Naca 65a004 Airfoil Section Mounted On A Body
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Author : Donald D. Arabian
language : en
Publisher:
Release Date : 1960
Investigation At Transonic Speeds Of Loading Over A 30 Deg Sweptback Wing Of Aspect Ratio 3 Taper Ratio 0 2 And Naca 65a004 Airfoil Section Mounted On A Body written by Donald D. Arabian and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960 with Aerodynamics, Transonic categories.
The aerodynamic load characteristics of a wing-body combination were determined experimentally at Mach numbers from 0.80 to 1.03 for angles of attack up to 26 degrees. Two wings, both with 30 degrees sweep of the quarter-chord line, taper ratio of 0.2, aspect ratio of 3, and thickness of 4 percent chord, but of different types of construction, were tested. One wing was of solid steel and the other was of plastic with an inner steel core ...
Reports And Memoranda
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Author :
language : en
Publisher:
Release Date : 1961
Reports And Memoranda 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 Aerodynamics categories.
An Investigation Of Wing And Aileron Loads Due To Deflected Inboard And Outboard Ailerons On A 4 Percent Thick 30 Degree Swepptback Wing At Transonic Speeds
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Author : Charles F. Whitcomb
language : en
Publisher:
Release Date : 1961
An Investigation Of Wing And Aileron Loads Due To Deflected Inboard And Outboard Ailerons On A 4 Percent Thick 30 Degree Swepptback Wing At Transonic Speeds written by Charles F. Whitcomb and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with categories.
U S Government Research Reports
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Author :
language : en
Publisher:
Release Date : 1961
U S Government Research 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 1961 with Science categories.