Contrails
The goal of the Contrails project is to help preserve and disseminate the technical record of 20th century aerospace research, highlighting in particular the research endeavors of the Illinois Tech community.

EASY-ACLS Dynamic Analysis Volume I - Component Mathematical Methods

Report Number: AFFDL TR 79-3105 Volume I
Author(s): M. K. Wahi; G. S. Duleba; J. R. Kilner; P. R. Perkins
Corporate Author: Boeing Aerospace Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1979-09
Pages: 248
Contract: F33615-77-C-3054
AD Number: ADA080634

Abstract:
Mathematical models were developed for a variety of Air Cushion Landing System components which include aircraft flight model components, wind, engine and air flow components, inelastic-elastic-trunk and cushion, air bag skid and arresting gear model components etc. The models were developed for utilization in the EASY-ACLS dynamic analysis computer program simulation.

Download this report

(PDF, 7.56 MB, 248 pages)

Other options for obtaining this report

Via the Defense Technical Information Center (DTIC):
A record for this report, and possibly a full-image download of the report, exists at DTIC

Via National Technical Information Service:
This report may have been digitized and made freely available for public download, or made publicly available for purchase by the National Technical Information Service through their online database, the National Technical Reports Library

Indications of Public Availability
No digital image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement

Related Reports

This report has the following parts/volumes: