DEVELOPMENT TEST SUMMARY IN SUPPORT OF X-20 ELEVON STRUCTURAL TEST PROGRAM

1966 ◽  
Author(s):  
John C. Grogan
Keyword(s):  
Test Program ◽  
Structural Test

Update of the Long-Term Inflow and Structural Test Program

2004 ◽  
Author(s):  
Herbert Sutherland ◽  
Jose Zayas ◽  
A. Sterns ◽  
Byron Neal
Keyword(s):  
Test Program ◽  
Structural Test

scholarly journals The long-term inflow and structural test program

2001 ◽  
Author(s):  
Herbert Sutherland ◽  
Perry Jones ◽  
Byron Neal
Keyword(s):  
Test Program ◽  
Structural Test

STRUCTURAL TEST PROGRAM F-106A AIRPLANE

1960 ◽  
Author(s):  
Sanford Lustig ◽  
David W. Jackson ◽  
Fred E. Hussong
Keyword(s):  
Test Program ◽  
Structural Test

Precision and bias in quantitative EDS: ASTM results

1992 ◽  
Vol 50 (2) ◽  
pp. 1654-1655
Author(s):  
John J. Friel
Keyword(s):  
Stainless Steel ◽  
Quantitative Analysis ◽  
Mechanical Alloy ◽  
Dead Time ◽  
Test Program ◽  
Round Robin Test ◽  
Wide Range ◽  
American Society ◽  
Takeoff Angle ◽  
Standardless Analysis

Committee E-04 on Metallography of the American Society for Testing and Materials (ASTM) conducted an interlaboratory round robin test program on quantitative energy dispersive spectroscopy (EDS). The test program was designed to produce data on which to base a precision and bias statement for quantitative analysis by EDS. Nine laboratories were sent specimens of two well characterized materials, a type 308 stainless steel, and a complex mechanical alloy from Inco Alloys International, Inconel® MA 6000. The stainless steel was chosen as an example of a straightforward analysis with no special problems. The mechanical alloy was selected because elements were present in a wide range of concentrations; K, L, and M lines were involved; and Ta was severely overlapped with W. The test aimed to establish limits of precision that could be routinely achieved by capable laboratories operating under real world conditions. The participants were first allowed to use their own best procedures, but later were instructed to repeat the analysis using specified conditions: 20 kV accelerating voltage, 200s live time, ∼25% dead time and ∼40° takeoff angle. They were also asked to run a standardless analysis.

Structural Foam Sheathing Test Program

AEI 2019 ◽  
2019 ◽  
Author(s):  
S. Shadravan ◽  
C. Ramseyer
Keyword(s):  
Test Program ◽  
Structural Foam
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