Analysis of Aircraft Simulations Using an Elliptic Cylinder and Multiple Plates.
Abstract
The aircraft simulation model developed under previous contract (N00019-77-0299) is extended in an attempt to study the pattern effects due to the presence of various substructures attached to an aircraft. A simple, efficient multiplate model is developed in that the various substructures, such as the jet engine housing, are treated simply by boxing-out the shape using multiple finite plates. This new numerical solution with second-order interaction GTD terms included shows excellent agreement when compared with the measured results. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Apr 01, 1979
- Accession Number
- ADA112783
Entities
People
- E. L. Pelton
- Nan Wang
- Walter Dennis Burnside
Organizations
- Ohio State University