Supersonic Lifting-Surface Computer Program for Cruciform Wing-Body Combinations.
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 Woodward's constant pressure panels to represent the wing. Such panels are also placed on the body surface to account for wing-body interference.
Document Details
- Document Type
- Technical Report
- Publication Date
- Dec 01, 1974
- Accession Number
- ADA003925
Entities
People
- Jack N. Nielsen
- Marnix F. E. Dillenius
Organizations
- Nielsen Engineering & Research (United States)