Aerodynamic Design: A Description of the Design Philosophy as it Applies to Wing, Flap, Engine Nacelles, Rear Fuselage, Tail Unit, Flying Controls and Performance

Author：  

Publisher： Emerald Group Publishing Ltd

ISSN： 0002-2667

Source： Aircraft Engineering, Vol.37, Iss.1, 1993-12, pp. : 6-8

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

Aerodynamic Design: A Description of the Design Philosophy as It Applies to Performance Requirements, Wings, Flaps, Engine Installations, Tail and Flying Controls

By A.F.R.Ae.S. B.J. Prior   B.Sc.(Eng.)   A.C.G.I.   D.I.C.  

Aircraft Engineering, Vol. 35, Iss. 5, 1993-12 ,pp. : 149-152

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

Part One—Design Philosophy and Systems: Choice of the Three Rear-Mounted Engine Configuration, and Description of the Basic Systems

By  

Aircraft Engineering, Vol. 34, Iss. 1, 1993-12 ,pp. : 2-6

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

Aerodynamic Design — Wing

By  

Aircraft Engineering, Vol. 41, Iss. 12, 1993-12 ,pp. : 30-36

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

Design and Fabrication of a Composite Rear Fuselage for the UH-60 Black Hawk

By Orlino Drew G.   Kay Bruce F.  

Journal of the American Helicopter Society, Vol. 28, Iss. 4, 1983-10 ,pp. : 8-13

AHS International

Access to resources Recommend Favorite

Aerodynamic Design and Performance

By  

Aircraft Engineering, Vol. 37, Iss. 8, 1993-12 ,pp. : 244-246

Emerald Group Publishing Ltd

Access to resources Recommend Favorite