Accession Number : ADA125764
Title : Wing-Alone Aerodynamic Characteristics to High Angles of Attack at Subsonic and Transonic Speeds.
Descriptive Note : Final technical rept. 1 Apr 79-15 Sep 82,
Corporate Author : NIELSEN ENGINEERING AND RESEARCH INC MOUNTAIN VIEW CA
Personal Author(s) : Briggs,M M ; Reed,R E ; Nielsen,J N
Report Date : Nov 1982
Pagination or Media Count : 358
Abstract : This report documents the results of a wind tunnel test conducted to determine the aerodynamic characteristics of unbanked wings from low to high angles of attack at subsonic and transonic speeds. Several wing models with differing planform geometry were tested. All wings were full-span with straight taper, zero trailing-edge sweep, constant bevel angle normal to all edges and constant thickness. The aerodynamic data obtained consisted of normal-force, axial-force, pitching-moment, yawing-moment, and semispan root bending-moment coefficients. Longitudinal, spanwise, and vertical aerodynamic centers of pressure were computed from the force and moment data.
Descriptors : *AERODYNAMIC CHARACTERISTICS , *WINGS , PITCH(MOTION) , YAW , ANGLE OF ATTACK , AERODYNAMIC LOADING , TRANSONIC FLIGHT , LEVEL FLIGHT , PRESSURE DISTRIBUTION , HIGH ANGLES , SUBSONIC FLIGHT
Subject Categories : Fluid Mechanics
Distribution Statement : APPROVED FOR PUBLIC RELEASE