columbus · A Study of Aerodynamic Control in Stalled Flight Long Laminar Separation Bubble Analysis

A Study of Aerodynamic Control in Stalled Flight Long Laminar Separation Bubble Analysis

Title: A Study of Aerodynamic Control in Stalled Flight Long Laminar Separation Bubble Analysis
Date: 1985
Index Abstract: Coming Soon
Photo Quality: Not Needed
Report Number: AFWAL TR 84-3091
Creator: Dvorak, F. A.; Choi, D. H.
Corporate Author: Analytical Methods, Inc.
Laboratory: Flight Dynamics Laboratory
Date Issued: 1985-02-01
Extent: 28
Identifier: ADA153850
Access Rights: Approved for public release; distribution unlimited.
Distribution Classification: 1
Contract: F33615-81-C-3626
DoD Project: 2307
DTIC Record Exists: No
Distribution Change Authority Correspondence: None
Abstract: This report describes an analysis method for laminar separation bubbles (long or short) on two-dimensional airfoil sections at incidence. A viscous/potential flow iterative procedure was chosen due to its simple and efficient nature. The boundary layer procedure is a finite-difference method, sometimes referred to as the 'Bosx Scheme', and uses the Cebeci-Smith two-layer, eddy viscosity model for turbulence closure. The potential flow calculation in such a way that it gives constant pressure along the surface inside the bubble, The coupled calculation procedure has been applied to the NACA 64A006 airfoil and satisfactory results have been obtained. Keywords: Panel methods; and Laminar separation bubble.
Report Availability: Full text available by request
Provenance: AFRL/VACA
Type: report
Format: 28 pages ; 28 cm.