Lift Correction for Finite Chord: A Method of Close Approximation that is not Laborious and is Applicable in General to Wings without Sweep

By D.Sc. J. Lockwood Taylor  

Aircraft Engineering, Vol. 22, Iss. 6, 1993-12 ,pp. : 174-174

Emerald Group Publishing Ltd

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Lift-Curve Slope at Subsonic and Supersonic Speeds: Graphical Presentation of Theoretical Results for Straight-Tapered Wings

By M.I.A.S. A. Stanbrook   B.Sc.  

Aircraft Engineering, Vol. 26, Iss. 8, 1993-12 ,pp. : 244-257

Emerald Group Publishing Ltd

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Establishment of Lift on an Aerofoil with a Jet Flap: A Theoretical Note Relating to a Wing with Trailing Edge Jet with Extension to Cover Wings of Finite Span

By Ingr.Dr. R. Hirsch  

Aircraft Engineering, Vol. 30, Iss. 1, 1993-12 ,pp. : 11-19

Emerald Group Publishing Ltd

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Establishment of Lift on an Aerofoil with a Jet Flap: A Theoretical Note Relating to a Wing with Trailing Edge Jet with Extension to Cover Wings of Finite Span

By Ingr.Dr R. Hirsch  

Aircraft Engineering, Vol. 29, Iss. 12, 1993-12 ,pp. : 366-375

Emerald Group Publishing Ltd

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The Calculation of Span Loadings: A Contribution to the Determination of the Distribution of Lift Across a Span by Successive Graphical Approximation

By Crean J.R.  

Aircraft Engineering, Vol. 9, Iss. 2, 1993-12 ,pp. : 45-50

Emerald Group Publishing Ltd

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