Fortran program for calculating the static longitudinal aerodynamic characteristics of wing-body-tail configurations including vortex lift from sharp edges

Dutt, HNV (1986) Fortran program for calculating the static longitudinal aerodynamic characteristics of wing-body-tail configurations including vortex lift from sharp edges. Technical Report. National Aeronautical Laboratory, Bangalore, India.

[img] PDF
tr_pd_ae_8613_R75207.pdf
Restricted to Repository staff only

Download (17MB)

Abstract

This project document is a User's manual for computer13; program for calculating the longitudinal aerodynamic13; characteristics of wing-body-tail combinations in subsonic flows and at angles of attack for which symmetrical pairs13; of vortices are shed from the body nose and leading edge13; and side edges of the lifting surfaces.13; This document contains a short description of the method,13; instructions for preparation of input and program listing.

Item Type: Monograph (Technical Report)
Uncontrolled Keywords: Vortex lattice method;Symmetrical vortex shedding;Suction analogy
Subjects: MATHEMATICAL AND COMPUTER SCIENCES > Computer Programming and Software
AERONAUTICS > Aerodynamics
Depositing User: Users 60 not found.
Date Deposited: 28 Aug 2006
Last Modified: 24 May 2010 04:18
URI: http://nal-ir.nal.res.in/id/eprint/2381

Actions (login required)

View Item View Item