Accession Number : ADA019222

Title :   Approximate Method of Calculating the Interaction of Finite-Span Airfoils in Unsteady Motion Above a Solid Surface (Priblizhennyi Metod Rascheta Vzaimodeistviya Krylev Konechnogo Razmakha pri Neustanovivshiemsya Dvizhenii nad Tverdoi Poverkhnostyu),

Corporate Author : NAVAL INTELLIGENCE SUPPORT CENTER WASHINGTON D C TRANSLATION DIV

Personal Author(s) : Treshkov,V. K.

Report Date : 26 NOV 1975

Pagination or Media Count : 9

Abstract : It is important for many practical problems to be able to analyze the aerodynamic characteris

Descriptors :   *Aerodynamic control surfaces, *Aerodynamic characteristics, Wings, Tail assemblies, Interactions, Ground level, Translations, USSR, Computations, Motion

Subject Categories : Aerodynamics
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE