Aeroplane Brake Development: An Examination of the Possibilities of Tandem Wheel Undercarriages Fitted with Brakes

By (France) R. Waring Brown   M.T.S.I.A.  

Aircraft Engineering, Vol. 6, Iss. 2, 1993-12 ,pp. : 49-50

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

The load on the brake parachute of a jet aeroplane under the influence of the engine wake

By SANDSTROM RUNE  

Aircraft Engineering, Vol. 43, Iss. 11, 1993-12 ,pp. : 26-30

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

Models in Aeroplane Design: Requirements for the Study of Strength, Stiffness and Aerodynamic Properties

By B.A. J. Taylor  

Aircraft Engineering, Vol. 12, Iss. 11, 1993-12 ,pp. : 322-328

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

A U.S. Government Specification: Details of Requirements in a 100 Horse-Power Two-Seater Aeroplane for Inspectors' Use

By  

Aircraft Engineering, Vol. 6, Iss. 8, 1993-12 ,pp. : 224-224

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

The Undercarriage in Aeroplane Project Design: A description of a method by which project engineers can assess the landing gear requirements of a particular design

By M.I.P.I. A. Cameron-Johnson   D.L.C.   M.I.E.D.  

Aircraft Engineering, Vol. 41, Iss. 2, 1993-12 ,pp. : 6-11

Emerald Group Publishing Ltd

Access to resources Recommend Favorite