Method for providing lateral control; control surfaces arranged so that they affect pressures over adjacent wings, and hence produce rolling moment; results of calculations and limited number of measurements which enable effectiveness of such controls to be estimated.
Lateral control at supersonic speeds by means of control surfaces on nacelles or on fuselage
Roy Aeronautical Soc -- J
Royal Aeronautical Society -- Journal ; 62 , n 570
1958
4 pages
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Fuselage Shape Optimization of a Wing-Body Configuration with Nacelles
Online Contents | 2003
|FUSELAGE SHAPE OPTIMIZATION AIMED AT WING-FUSELAGE CONFIGURATION DRAG REDUCTION AT SUPERSONIC SPEEDS
DOAJ | 2017
|