000 00512pam a2200157a 44500
082 _aTR
_bTND-7752
100 _aMiller,Charles G.
245 1 _aPROGRAM AND CHARTS FOR DETERMINING SHOCK TUBE EXPANSION TUBE AND EXPANSION TUNNEL FLOW QUANTITIES FOR REAL AIR
260 _a
_bNasa, Washington, D.C.
_c1975
300 _a278
440 _aNational Aeronautics And Space Administration
_vTnd-7752
500 _aBound With: Nasa Tnd-7736-7752
700 _aWilder,Sue E.
964 _gCIRC
997 _aTR2496 C
999 _c392679
_d392679