Accession Number:

ADA003925

Title:

Supersonic Lifting-Surface Computer Program for Cruciform Wing-Body Combinations.

Descriptive Note:

Technical rept. 1 Oct 73-30 Sep 74,

Corporate Author:

NIELSEN ENGINEERING AND RESEARCH INC MOUNTAIN VIEW CALIF

Report Date:

1974-12-01

Pagination or Media Count:

138.0

Abstract:

A lifting-surface computer program has been written for supersonic cruciform wing-body combinations at combined pitch and yaw conditions. The method involves supersonic line sources and doublets to model the body and uses Woodwards constant pressure panels to represent the wing. Such panels are also placed on the body surface to account for wing-body interference.

Subject Categories:

  • Guided Missile Dynamics, Configurations and Control Surfaces

Distribution Statement:

APPROVED FOR PUBLIC RELEASE