Theoretical Distribution Of Load Over A Swept Back Wing

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Theoretical Distribution Of Load Over A Swept Back Wing

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Author : Doris Cohen
language : en
Publisher:
Release Date : 1942

Theoretical Distribution Of Load Over A Swept Back Wing written by Doris Cohen and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1942 with Aerodynamic load categories.

The load over an elliptical wing with 30 degrees sweepback has been calculated by a method, based on vortex theory, which takes account of the chordwise distribution of lifting area. The theory indicates a 14-percent loss in total lift due to the introduction of sweepback, with the greatest loss taking place at the center of the span. An increase in concentration of load at the tips is also indicated. The results are compared with the results previously obtained by somewhat simpler calculations based on the assumption of a single lifting vortex.

Theoretical Loading At Supersonic Speeds Of Flat Swept Back Wings With Interacting Trailing And Leading Edges

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Author : Doris Cohen
language : en
Publisher:
Release Date : 1949

Theoretical Loading At Supersonic Speeds Of Flat Swept Back Wings With Interacting Trailing And Leading Edges written by Doris Cohen and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1949 with Aerodynamic load categories.

By the method of superposition of conical flows, the load distribution is calculated for regions of a long swept-back wing behind the points at which the Mach lines from the trailing-edge apex intersect the leading edge. It is found that a good approximation on the load can be obtained by the application of a fairly simple correction factor to the two-dimensional subsonic distribution. The similarity of two-dimensional flow is used to derive expressions for the loss of lift behind the Mach lines from the tips of the wing.

Linearized Lifting Surface Theory For Swept Back Wings With Slender Plan Forms

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Author : Harvard Lomax
language : en
Publisher:
Release Date : 1949

Linearized Lifting Surface Theory For Swept Back Wings With Slender Plan Forms written by Harvard Lomax and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1949 with Aerodynamic load categories.

The spanwise and chordwise distribution of loading, the lift, and the induced drag of a swept-back wing of slender plan form are developed by means of linearized lifting-surface theory. The results are applicable for all free-stream Mach numbers. The term slender implies that the ratio of the reduced span to over-all length of the wing is small.

The Calculation Of Span Load Distributions On Swept Back Wings

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Author : William Mutterperl
language : en
Publisher:
Release Date : 1941

The Calculation Of Span Load Distributions On Swept Back Wings written by William Mutterperl and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1941 with Airplanes categories.

Span load distributions of swept-back wings have been calculated. The method used was to replace the wing with a bound vortex at the quarter-chord line and to calculate the downwash due to the system of bound and trailing vortices to conform at the three-quarter-chord line to the slope of the flat-plate wing surface. Results are given for constant-chord and 5:1 tapered plan forms, for swee-pback angles of 0, 30 and 45 degresss, and for aspect ratios of 3, 6, and 9. Some comments on the stalling of swept-back wings are included.

Theoretical Calculation Of The Pressure Distribution Span Loading And Rolling Moment Due To Sideslip At Supersonic Speeds For Thin Sweptback Tapered Wings With Supersonic Trailing Edges And Wing Tips Parallel To The Axis Of Wing Symmetry

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Author : Kenneth Margolis
language : en
Publisher:
Release Date : 1953

Theoretical Calculation Of The Pressure Distribution Span Loading And Rolling Moment Due To Sideslip At Supersonic Speeds For Thin Sweptback Tapered Wings With Supersonic Trailing Edges And Wing Tips Parallel To The Axis Of Wing Symmetry written by Kenneth Margolis 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.

Wing Load Distribution On A Swept Wing Airplane In Flight At Mach Numbers Up To 1 11 And Comparison With Theory

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Author : L. Stewart Rolls
language : en
Publisher:
Release Date : 1952

Wing Load Distribution On A Swept Wing Airplane In Flight At Mach Numbers Up To 1 11 And Comparison With Theory written by L. Stewart Rolls and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1952 with categories.

Wartime Report

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Author :
language : en
Publisher:
Release Date : 1943

Wartime Report written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1943 with Aeronautics categories.

Reproductions of reports, some declassified, of research done at Langley Memorial Aeronautical Laboratory during World War II. The order of reports does not represent when they were chronologically issued. Reference to the original version of each report is included.

Naca Wartime Report

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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date :

Naca Wartime Report written by United States. National Advisory Committee for Aeronautics and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on with Aeronautics categories.

Wartime Report

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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date :

Wartime Report written by United States. National Advisory Committee for Aeronautics and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on with Aeronautics categories.

Annual Report Of The National Advisory Committee For Aeronautics

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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1950

Annual Report Of The National Advisory Committee For Aeronautics written by United States. National Advisory Committee for Aeronautics and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1950 with Aeronautics categories.

Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.