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.