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L. D. Kayser
发表
Wind Tunnel Tests on a Nonaxisymmetric Projectile Shape at Mach Numbers 2.5 to 6.0.
L. D. Kayser, 1983 .
Microphone Coverings for a Helicopter Mounted Acoustic Locator.
L. D. Kayser, J. H. Spurk, 1969 .
PRESSURE DISTRIBUTION, HEAT TRANSFER, AND DRAG TESTS ON THE GOODYEAR BALLUTE AT MACH 10
L. D. Kayser, 1962 .