The Stalling of Tapered Wings: Puzzling Results with Two Junkers Wings of Different Plan

Author：

ISSN： 0002-2667

Source： Aircraft Engineering, Vol.9, Iss.11, 1993-12, pp. : 285-286

Disclaimer: Any content in publications that violate the sovereignty, the constitution or regulations of the PRC is not accepted or approved by CNPIEC.

Previous Menu Next

Abstract

Related content

Some Notes on Tapered Wings: The Effects of Brake Flaps, Taper and "Sweep" on Stalling

By F.R.Ae.S. H.B. Irving B.Sc.

Aircraft Engineering, Vol. 9, Iss. 2, 1993-12 ,pp. : 31-36

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

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

Access to resources Recommend Favorite

Dunlop Aviation Spreads its Wings

Aircraft Engineering, Vol. 56, Iss. 5, 1993-12 ,pp. : 6-7

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

Aircraft Wings Ride on Flexello Castors

Aircraft Engineering, Vol. 62, Iss. 5, 1993-12 ,pp. : 17-17

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

An Unconventional Monoplane: A Low-Wing Four-Seater with Mono-Spar Wings and Fuselage and Two Pobjoy Engines

Aircraft Engineering, Vol. 4, Iss. 5, 1993-12 ,pp. : 111-111

Emerald Group Publishing Ltd

Access to resources Recommend Favorite