Accession Number : AD0700822

Title :   WING-EDGE PIVOT POINTS IN SUBSONIC LIFTING SURFACE ANALYSIS,

Corporate Author : MARTIN MARIETTA CORP BALTIMORE MD RESEARCH INST FOR ADVANCED STUDIES

Personal Author(s) : Jordan,Peter F.

Report Date : NOV 1969

Pagination or Media Count : 20

Abstract : An elementary and instructive method is described for deriving formulas for the spanwise singularities. Prior results are reviewed, and additional terms are given. (Author)

Descriptors :   (*AERODYNAMIC CONTROL SURFACES, SUBSONIC CHARACTERISTICS), LIFT, LEADING EDGES, ASPECT RATIO, TRAILING EDGE, DOWNWASH, PRESSURE, DISTRIBUTION, MATHEMATICAL ANALYSIS

Subject Categories : Aerodynamics
      Aircraft
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE