Effect of forward velocity on sound-pressure level in the near noise field of a moving jet (NASA TN D-61)
By: National Aeronautics and Space Administration.
Material type:
BookPublisher: Washington NASA 1959Technical note NASA TN D-62 to NASA TN D-70 are bound with Acc. No. 63632
NASA TN D-62 -- Analysis of the transient radiation heat transfer of an uncooled rocket engine operating outside earth's atmosphere/ William H. Robbins.-- NASA TN D-63 -- Field experiments on treatment of fluorine spills with water or soda ash/ R. James Rollbuhler, George R. Kinney and Lorenz C. Leopold .--NASA TN D-64 -- Graphical rajectory analysis/ Aaron S. Boksenbom .-- NASA TN D-65 -- Propellant vaporization as a criterion for rocket-engine design; experimental effect of chamber diameter on liquid oxygen - heptane performance/ Marcus F. Heidmann .-- NASA TN D-66 -- Analysis of effects of rocket-engine design parameters on regenerative-cooling capabilities of several propellants/ Arthur N. Curren, Harold G. Price and Howard W. Douglass .-- NASA TN D-67 -- Blowoff of propane and hydrogen diffusion flames at high mach number, ramjet conditions/ R. J. Bacigalupi and E. A. Lezberg .-- NASA TN D-68 -- General-purpose subroutines for the IBM 650 magnetic drum data-processing machine with attachments/ Vearl N. Huff, Don N. Turner and Oliver W. Reese .-- NASA TN D-69 -- Thermal fatigue of ductile materials III - Behavior of crucible 422 steel/ Francis J. Clauss .-- NASA TN D-70 -- Gravity torque on an orbiting vehicle/ Brian F. Doolin
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