Dynamic response of rising and falling balloon wind sensors with application to estimates of wind loads on launch vehicles

By Reed, Wilmer H.. Washington NASA 1963 . various pagings

Pressure distributions on two-dimensional sharp-leading-edge flat plates with sweep angles of 0 degree,30 degree,and 45 degree at a mach number of 6 and angles of attack from 0 degree to 90 degree[NASA TN D-1371]

By Hondros,James G.. Washington National aeronautics and space adminstration 1962 . 23p , Bound vol. contains D 1371- 1375