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Three-dimensional, Unsteady-lift Problems in High-speed Flight

Three-dimensional, Unsteady-lift Problems in High-speed Flight
Author: Harvard Lomax
Publisher:
Total Pages: 48
Release: 1950
Genre: Boundary value problems
ISBN:

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The problem of the build-u of lift on two- and three-dimensional wings flying at high speeds is discussed as a boundary-value problem for the classical wave equation. Kirchhoff's formula is applied so that the analysis is reduced, just as in the steady state, to an investigation of sources and doublets. Some simple applications of this method are considered, including the determination of the starting lift of a three-dimensional wing and the potential functions for some types of unsteady vortex motion.


Three-dimensional Unsteady Lift Problems in High-speed Flight

Three-dimensional Unsteady Lift Problems in High-speed Flight
Author: Harvard Lomax
Publisher:
Total Pages: 72
Release: 1951
Genre: Airplanes
ISBN:

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The indicial lift and pitching-moment coefficients are derived for flat-plate triangular wings at supersonic speeds. Coefficients are determined for angle-of-attack distributions corresponding to sinking and pitching wings. The wing with supersonic edges is completely analyzed, the wing with subsonic edges is partially analyzed; the solution in this case being completed for very narrow wings by an application of slender wing theory. In case of the supersonic edges, a comparison is made with known two-dimensional results and also with results for the same triangular wing in reversed flow.


Three-Dimensional Unsteady Lift Problems in High-Speed Flight-The Triangular Wing

Three-Dimensional Unsteady Lift Problems in High-Speed Flight-The Triangular Wing
Author:
Publisher:
Total Pages: 42
Release: 1950
Genre:
ISBN:

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The problem of the build-up of lift on two- and three-dimensional wings flying at high speeds is discussed as a boundary-value problem for the classical wave equation. Kirchhoff's formula is applied so that the analysis is reduced, Just as in the steady state, to an investigation of sources' and doublets. Some simple applications of this method are considered, including the determination of the starting lift of a three- dimensional wing and the potential functions for some types of unsteady vortex motion.


Adventures in Research

Adventures in Research
Author: Edwin Phelps Hartman
Publisher:
Total Pages: 580
Release: 1970
Genre: Aeronautics
ISBN:

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Annual Report

Annual Report
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Total Pages: 534
Release: 1953
Genre: Aeronautics
ISBN:

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Aeroelasticity

Aeroelasticity
Author: Raymond L. Bisplinghoff
Publisher: Courier Corporation
Total Pages: 886
Release: 1996-01-01
Genre: Technology & Engineering
ISBN: 9780486691893

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Highly regarded text deals with aeroelasticity as well as underlying aerodynamic and structural tools. Topics include incompressible flow, flutter, model theory, and much more. Over 300 illustrations. 1955 edition.


Report

Report
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Total Pages: 78
Release: 1952
Genre: Aeronautics
ISBN:

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Annual Report of the National Advisory Committee for Aeronautics

Annual Report of the National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Total Pages: 1200
Release: 1954
Genre: Aeronautics
ISBN:

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