Span Loadings Due To Wing Twist At Transonic And Supersonic Speeds

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Span Loadings Due to Wing Twist at Transonic and Supersonic Speeds

Frederick C. Grant
Span Loadings Due to Wing Twist at Transonic and Supersonic Speeds Book PDF

Author : Frederick C. Grant
Publisher : Unknown
Page : 18 pages
File Size : 44,9 Mb
Release : 1957
Category : Aerodynamic load
ISBN : UOM:39015086466110

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Span Loadings Due to Wing Twist at Transonic and Supersonic Speeds by Frederick C. Grant Pdf

Two similar tapered sweptback plan forms with the same two spanwise variations of twist have been tested in the Mach number range from 0.8 to 2.0. The test results showed, in general, rather good agreement with theoretical predictions of the incremental span loadings due to twist for zero angle of attack. The measured incremental span loadings due to twist generally diminished with increasing angle of attack through the Mach number range. At a Mach number of 0.9, the incremental loadings progressively vanished from the tip inboard with increasing angle of attack. For the highest angles of attack (about 20 degrees) at Mach number 0.9, there was no difference in the span loadings of the flat and twisted wings. At a higher supersonic speeds, a similar vanishing at the tips of the incremental loading due to twist was starting at the highest angles of attack (near 20 degrees).

Index of N A S A Technical Publications

United States. National Aeronautics and Space Administration
Index of N A S A Technical Publications Book PDF

Author : United States. National Aeronautics and Space Administration
Publisher : Unknown
Page : 210 pages
File Size : 52,6 Mb
Release : 1958
Category : Electronic
ISBN : OSU:32435060228327

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Index of N A S A Technical Publications by United States. National Aeronautics and Space Administration Pdf

Index to NASA Technical Publications

United States. National Aeronautics and Space Administration
Index to NASA Technical Publications Book PDF

Author : United States. National Aeronautics and Space Administration
Publisher : Unknown
Page : 208 pages
File Size : 47,6 Mb
Release : 1959
Category : Electronic
ISBN : STANFORD:36105024165693

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Index to NASA Technical Publications by United States. National Aeronautics and Space Administration Pdf

Monthly Catalog of United States Government Publications

United States. Superintendent of Documents
Monthly Catalog of United States Government Publications Book PDF

Author : United States. Superintendent of Documents
Publisher : Unknown
Page : 1284 pages
File Size : 43,9 Mb
Release : 1961
Category : Government publications
ISBN : WISC:89038149274

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Monthly Catalog of United States Government Publications by United States. Superintendent of Documents Pdf

Monthly Catalog of United States Government Publications, Cumulative Index

United States. Superintendent of Documents
Monthly Catalog of United States Government Publications Cumulative Index Book PDF

Author : United States. Superintendent of Documents
Publisher : Unknown
Page : 1366 pages
File Size : 48,6 Mb
Release : 1968
Category : United States
ISBN : STANFORD:36105022657535

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Monthly Catalog of United States Government Publications, Cumulative Index by United States. Superintendent of Documents Pdf

NASA Technical Note

Anonim
NASA Technical Note Book PDF

Author : Anonim
Publisher : Unknown
Page : 750 pages
File Size : 52,8 Mb
Release : 1962
Category : Electronic
ISBN : MINN:31951000845778F

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NASA Technical Note by Anonim Pdf

A Tabulation of Section Aerodynamic Characteristics at Mach Numbers of 1.61 and 2.01 for Four Swept Wings Having the Same Planform But Different Surface Shapes

Emma Jean Landrum
A Tabulation of Section Aerodynamic Characteristics at Mach Numbers of 1 61 and 2 01 for Four Swept Wings Having the Same Planform But Different Surface Shapes Book PDF

Author : Emma Jean Landrum
Publisher : Unknown
Page : 40 pages
File Size : 53,8 Mb
Release : 1962
Category : Airplanes
ISBN : UIUC:30112106593137

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A Tabulation of Section Aerodynamic Characteristics at Mach Numbers of 1.61 and 2.01 for Four Swept Wings Having the Same Planform But Different Surface Shapes by Emma Jean Landrum Pdf

A Tabulation of Wind-tunnel Pressure Data and Section Aerodynamic Characteristics at Mach Numbers of 1.61 and 2.01 for a Reflex Cambered Wing and a Cambered and Twisted Wing Having the Same Swept Planform

Emma Jean Landrum
A Tabulation of Wind tunnel Pressure Data and Section Aerodynamic Characteristics at Mach Numbers of 1 61 and 2 01 for a Reflex Cambered Wing and a Cambered and Twisted Wing Having the Same Swept Planform Book PDF

Author : Emma Jean Landrum
Publisher : Unknown
Page : 76 pages
File Size : 44,9 Mb
Release : 1962
Category : Aerofoils
ISBN : UIUC:30112106873331

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A Tabulation of Wind-tunnel Pressure Data and Section Aerodynamic Characteristics at Mach Numbers of 1.61 and 2.01 for a Reflex Cambered Wing and a Cambered and Twisted Wing Having the Same Swept Planform by Emma Jean Landrum Pdf

Technical Abstract Bulletin

Defense Documentation Center (U.S.)
Technical Abstract Bulletin Book PDF

Author : Defense Documentation Center (U.S.)
Publisher : Unknown
Page : 1116 pages
File Size : 54,6 Mb
Release : 1961-02
Category : Technology
ISBN : UTEXAS:059172131213000

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Technical Abstract Bulletin by Defense Documentation Center (U.S.) Pdf

NASA SP.

Anonim
NASA SP Book PDF

Author : Anonim
Publisher : Unknown
Page : 464 pages
File Size : 53,6 Mb
Release : 1962
Category : Aeronautics
ISBN : UOM:39015057253554

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NASA SP. by Anonim Pdf

Loads on External Stores at Transonic and Supersonic Speeds

Lawrence Duncan Guy
Loads on External Stores at Transonic and Supersonic Speeds Book PDF

Author : Lawrence Duncan Guy
Publisher : Unknown
Page : 16 pages
File Size : 55,5 Mb
Release : 1955
Category : Aerodynamic load
ISBN : UOM:39015095100908

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Loads on External Stores at Transonic and Supersonic Speeds by Lawrence Duncan Guy Pdf

Results of recent wind-tunnel investigations of the loads on external stores at transonic and supersonic speeds have shown that the most critical store loading appears to be that due to the store side force, both because of its magnitude and because the force acts in the direction of the least structural strength of the pylon. The magnitude of the side forces is determined principally by angle of attack, store position, and Mach number. Angle of attack and store positions are inextricably related since the rate of change of side force with angle of attack, which can be very large, is primarily a function of position. Also, at moderate angles of attack, the rate of increase of side-force coefficient with angle of attack for a given store position is essentially constant with Mach number. The effects of Mach number are shown principally in the values of the coefficient at small angles of attack. These values are strongly influenced by local angularities and the changes in flow behavior that occur at transonic and supersonic speeds.