Air-Cushion Pressure During Stiff-Operation for Air-Cushion Landing Systems. Part II. Experiments.

Item

Title
Air-Cushion Pressure During Stiff-Operation for Air-Cushion Landing Systems. Part II. Experiments.
Date
1972
Index Abstract
Not Available
Photo Quality
Complete
Report Number
AFFDL TR 71-4 Part 2
Corporate Author
Ohio State Univ Research Foundation Columbus
Extent
104
Identifier
AD0750936
Access Rights
Approved for public relaease; distribution unlimited
Distribution Classification
1
DTIC Record Exists
No
Distribution Change Authority Correspondence
None
Date Modified
Scanned by request 11/7/2005 submitted by a Private Citizen (No Known Affiliation)
Abstract
The report describes the experimental verification of the theory developed in Part I for ACLS in its stiff-mode operation. It also reports the discharge coefficient data required for computing air flow requirements. At low ground clearances, the theory was verified to be in excellent agreement with the experimental data obtained. At higher values of the ground clearance where the viscous flow theory is not expected to hold, appreciable difference between the experimental data and theoretical computation was observed. A multi-jet theory yet to be developed is expected to bridge the gap.
Report Availability
Full text available
Date Issued
1972-03
Provenance
Lockheed Martin Missiles & Fire Control
Type
report
Format
1 online resource
Creator
Han, Lit S.