Title

EASY-ACLS Dynamic Analysis Volume I - Component Mathematical Methods

Date

1979

Index Abstract

Not Available

Photo Quality

Not Needed

Report Number

AFFDL TR 79-3105 Volume I

Creator

Wahi, M. K.

Kilner, J. R.

Perkins, P. R.

Duleba, G. S.

Corporate Author

Boeing Aerospace Company

Laboratory

Air Force Flight Dynamics Laboratory

Extent

248

Identifier

ADA080634

ADA080634

Access Rights

Approved for public release; distribution is unlimited

Distribution Classification

1

Contract

F33615-77-C-3054

DTIC Record Exists

Yes

Distribution Conflict

No

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.

Report Availability

Full text available

Date Issued

1979-09

Publisher

Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command

Date Modified

Scanned by request 3/2/2018 submitted by Private Citizen (No Known Affiliation)

Provenance

Bombardier/Aero

Type

report

Format

1 online resource