An Analysis of Amplitude Probability Measurements

Item

Title
An Analysis of Amplitude Probability Measurements
Date
1965
Index Abstract
Coming Soon
Photo Quality
Not Needed
Report Number
FDL TDR 64-116
Creator
Thrall, G. P.
Corporate Author
Measurement Analysis Corporation
Laboratory
Air Force Flight Dynamics Laboratory
Extent
38
Identifier
AD0617611
Access Rights
Notice(s)
Distribution Classification
1
Contract
AF 33(615)-1418
DoD Project
1370
DoD Task
137005
DTIC Record Exists
No
Distribution Change Authority Correspondence
None
Abstract
Six-component force and moment data were obtained for Mach 5 and 8 flows over a blunt pyramidal configura tion. The model had a triangular cross section and was composed of two dihedral surfaces and a 70-degree sweepback delta wing lower surface. Three-component force and moment data were obtained on a remotely controlled trailing edge flap at deflections up to 40 degrees. All three surfaces had trailing edge flaps and the model was tested with and without canards and a ventral fin. The model was pitched at angles of attack between =54 degrees and side-slip angles between -4 and +14 degrees. For both Mach numbers, the data were obtained for a nominal free stream Reynolds number, based on model length, of 4.5 million. Selected configurations were tested at other Reynolds numbers between 1.2 and 9.1 million.
Report Availability
Full text available
Date Issued
1965-03
Provenance
Lockheed Martin Missiles & Fire Control
Type
report
Format
1 online resource
Media
FDLTDR64-116.pdf