Accession Number : ADA280225


Title :   Handbook of Supersonic Aerodynamics. Section 18. Shock Tubes


Corporate Author : BUREAU OF NAVAL WEAPONS WASHINGTON DC


Personal Author(s) : Glass, I I ; Hall, J G


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/a280225.pdf


Report Date : Dec 1959


Pagination or Media Count : 634


Abstract : Contents: Performance of Simple Constant-Area Shock tubes; Observed flows in a constant-area shock tube; Production of strong shock waves; Application of the shock tube; Shock-tube materials; Design and Construction; and shock-tube.


Descriptors :   *SHOCK TUBES , *SUPERSONIC FLOW , TEMPERATURE , OPTICAL DETECTION , SHOCK WAVES , LIGHT , GAS DYNAMICS , PRESSURE , BOUNDARY LAYER TRANSITION , HANDBOOKS , AEROTHERMODYNAMICS , WIND TUNNELS , BOUNDARY LAYER FLOW , RAREFACTION , HEAT TRANSFER , DENSITY


Subject Categories : Test Facilities, Equipment and Methods
      Fluid Mechanics


Distribution Statement : APPROVED FOR PUBLIC RELEASE