On the exact solution of the linearized lifting-surface problem of an elliptic wing

A. Hauptman; T. Miloh

doi:10.1093/qjmam/39.4.580

On the exact solution of the linearized lifting-surface problem of an elliptic wing

A. Hauptman^*, T. Miloh

^*Corresponding author for this work

School of Mechanical Engineering

Tel Aviv University

Research output: Contribution to journal › Comment/debate

1 Scopus citations

Abstract

Equation (40):. x2=h-2(1-h2)-2(ρ2-h2)(μ2-h2)(h2-v2),z2=(1-h2)-2(ρ2-1)(1-μ2)(1-v2).Last line of page 49:. ...σ varying between unity and infinity.... page 50:. M(λ)=|λ2-1|12M¯(λ).Equation (51):. g2nm=N¯2nm(ρ=1)N¯2nm(μ)N¯2nm(v).Equation (65a) (pages 54 and 55):. CL/α=4(1-h2)12[1+E2(h)/(1+1-h2h1n1+h(1-h2)12)]-1.

Original language	English
Pages (from-to)	580
Number of pages	1
Journal	Quarterly Journal of Mechanics and Applied Mathematics
Volume	39
Issue number	4
DOIs	https://doi.org/10.1093/qjmam/39.4.580
State	Published - Nov 1986

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title = "On the exact solution of the linearized lifting-surface problem of an elliptic wing",

abstract = "Equation (40):. x2=h-2(1-h2)-2(ρ2-h2)(μ2-h2)(h2-v2),z2=(1-h2)-2(ρ2-1)(1-μ2)(1-v2).Last line of page 49:. ...σ varying between unity and infinity.... page 50:. M(λ)=|λ2-1|12M¯(λ).Equation (51):. g2nm=N¯2nm(ρ=1)N¯2nm(μ)N¯2nm(v).Equation (65a) (pages 54 and 55):. CL/α=4(1-h2)12[1+E2(h)/(1+1-h2h1n1+h(1-h2)12)]-1.",

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T1 - On the exact solution of the linearized lifting-surface problem of an elliptic wing

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AU - Miloh, T.

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N2 - Equation (40):. x2=h-2(1-h2)-2(ρ2-h2)(μ2-h2)(h2-v2),z2=(1-h2)-2(ρ2-1)(1-μ2)(1-v2).Last line of page 49:. ...σ varying between unity and infinity.... page 50:. M(λ)=|λ2-1|12M¯(λ).Equation (51):. g2nm=N¯2nm(ρ=1)N¯2nm(μ)N¯2nm(v).Equation (65a) (pages 54 and 55):. CL/α=4(1-h2)12[1+E2(h)/(1+1-h2h1n1+h(1-h2)12)]-1.

AB - Equation (40):. x2=h-2(1-h2)-2(ρ2-h2)(μ2-h2)(h2-v2),z2=(1-h2)-2(ρ2-1)(1-μ2)(1-v2).Last line of page 49:. ...σ varying between unity and infinity.... page 50:. M(λ)=|λ2-1|12M¯(λ).Equation (51):. g2nm=N¯2nm(ρ=1)N¯2nm(μ)N¯2nm(v).Equation (65a) (pages 54 and 55):. CL/α=4(1-h2)12[1+E2(h)/(1+1-h2h1n1+h(1-h2)12)]-1.

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On the exact solution of the linearized lifting-surface problem of an elliptic wing

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