Force and Pressure Tests of an Agard Calibration Model B at a Mach Number of 10

Item

Title
Force and Pressure Tests of an Agard Calibration Model B at a Mach Number of 10
Date
1964
Index Abstract
Coming Soon
Photo Quality
Not Needed
Report Number
AEDC TDR 64-31
Creator
Matthews, R. K.
Trimmer, L. L.
Corporate Author
ARO, Inc.
Extent
28
Identifier
AD0430701
Distribution Classification
1
Contract
AF 40(600)-1000
DoD Project
None Given
DoD Task
None Given
DTIC Record Exists
No
Distribution Change Authority Correspondence
None
Abstract
The AGARD Calibration Model B, with and without wings, was tested at a nominal Mach number of 10. Force and moment coefficients were obtained over a range of pitch and yaw angles from -5 to 15.5 degrees with a Reynolds number range from 1.10 x 10 to the 6th power to 9.80 x 10 to the 6th power, based on model length. The lift-curve slope, aerodynamic center, and drag coefficients show excellent correlation with data from other tunnels at various Mach numbers.
Report Availability
Full text available by request
Date Issued
1964-02
Publisher
Arnold Air Force Station, TN : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force
Provenance
IIT
Type
report
Format
28 pages ; 28 cm.