Accession Number : AD0740369
Title : Analytical Investigation of Variable Camber Concepts.
Descriptive Note : Final rept. 15 Jan-15 Aug 71,
Corporate Author : BOEING CO SEATTLE WASH AERONAUTICAL AND INFORMATION SYSTEMS DIV
Personal Author(s) : DE Costa,A. Larry ; Ishimitsu,Kichio K. ; Pickrel,Charles R. ; Miller,Douglas S. ; Zierten,Thomas A.
Report Date : DEC 1971
Pagination or Media Count : 169
Abstract : The principal objective of the investigation was to determine analytically the potential aerodynamic performance improvements that may be achieved through the use of variable camber. The feasibility study considered initially systematic camber variations on two-dimensional airfoils representative of successful airfoils in widespread current usage and of a most promising research airfoil. The application of variable camber to each of these airfoils resulted in significant expansions of their performance envelopes. It was found that the 'Whitcomb Supercritical Airfoil' achieved outstanding aerodynamic performance throughout the speed regime studied. (Author)
Descriptors : (*AIRFOILS, CAMBER), AERODYNAMIC CONTROL SURFACES, FEASIBILITY STUDIES, PERFORMANCE(ENGINEERING), PATROL AIRCRAFT, SWEPTBACK WINGS, JET FIGHTERS, ATTACK BOMBERS
Subject Categories : Bombers
Attack and Fighter Aircraft
Distribution Statement : APPROVED FOR PUBLIC RELEASE