[1]
Hsu, D, Barnard, D, Peters, J, Dayal, V, 2000, Physical basis of tap test as a quantitative imaging tool for composite structures on aircraft, Rev. Prog. Quantitative NDE, Vol. 19, eds. D. O. Thompson and D. E. Chimenti, Amer. Inst. Phys. Melville, New York. pp.1857-1864.
DOI: 10.1063/1.1306256
Google Scholar
[2]
Peters, J, Barnard, D, Hudelson, N, Simpson, T, Hsu, D, 2000, A prototype tap testing imaging system: Initial field test results, Rev. Prog. Quantitative NDE, Vol. 19, eds. D. O. Thompson and D. E. Chimenti, Amer. Inst. Phys. Melville, New York. p.2053-(2060).
Google Scholar
[3]
Barnard, D, Peters, J, Hsu, D, 2001, Development of a magnetic cam for the computer aided tap test system, Rev. Prog. Quantitative NDE, Vol. 20, eds. D. O. Thompson and D. E. Chimenti, Amer. Inst. Phys. Melville, New York. p.1966-(1971).
Google Scholar
[4]
Peters, J, Nielsen, Z, Hsu, D, 2001, Comparison of local stiffness of composite honeycomb sandwich structures measured by tap test and mechanical test, Rev. Prog. Quantitative NDE, Vol. 20, eds. D. O. Thompson and D. E. Chimenti, Amer. Inst. Phys. Melville, New York. pp.1031-1038.
DOI: 10.1063/1.1373868
Google Scholar
[5]
Air coupled ultrasonic system provided by QMI, Inc., Costa Mesa, CA. min max Transmitted Amplitude.
Google Scholar