Accession Number:

ADP006071

Title:

Experiences Using the MARK IV Supersonic Hypersonic Arbitrary Body Program,

Descriptive Note:

Corporate Author:

BRITISH AEROSPACE PLC BRISTOL (UNITED KINGDOM)

Personal Author(s):

Report Date:

1987-11-01

Pagination or Media Count:

18.0

Abstract:

This paper describes work done during the last two years in an attempt to gain an understanding of, and to establish a capability for the use of, the Douglas SupersonicHypersonic Arbitrary Body Program SHABP. The program has a complex structure and offers a large variety of aerodynamic prediction methods to solve many different types of problem. Most of the features of the program have been used with some success. Aspects of the flowfield routines and viscous options, which could not be utilised correctly, are either under investigation, or updates to the programming are awaited. Some accurate predictions have been made using the inviscid pressure methods, which have been evaluated for a wide range of configurations, for Mach Numbers from 1.7 to 25.0 and from an incidence of -8 to 40 deg. The code has been seen to be highly flexible, but the accuracy of the results is user dependent. Relative to computational fluid dynamics codes, SHABP geometries are easy to prepare and the code is cheap to run.

Subject Categories:

  • Fluid Mechanics
  • Research and Experimental Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE