Accession Number:

ADA045621

Title:

User's Guide to Computer Program for Estimating Airplane Local Flow Field Due to Wing-Body Effects.

Descriptive Note:

Phase rept.,

Corporate Author:

NAVAL AIR DEVELOPMENT CENTER WARMINSTER PA AIR VEHICLE TECHNOLOGY DEPT

Personal Author(s):

Report Date:

1977-04-01

Pagination or Media Count:

20.0

Abstract:

This report describes a computer program, and its use, which has been written to determine, using a relatively simple model, the local flow field about an airplane due to wing-body effects. The program includes compressibility effects up to the critical Mach number. It takes as inputs various geometric parameters and the flight condition in terms of Mach number, lift coefficient, and angle of attack. Author

Subject Categories:

  • Computer Programming and Software
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE