000			02090nam a22003017a 4500
003			OSt
005			20220816134547.0
008			220712b xxu||||| |||| 00| 0 eng d
040			_cIIT Kanpur
041			_aeng
110			_aWashington: National Aeronautics and Space Administration
245			_aNASA technical note [NASA TN D 161-170]
260			_aWashington, D. C. _bNational Aeronautics and Space Administration _c1959
440			_aNational Aeronautics and Space Administration
440			_aNASA Technical note
500			_aNASA TN D-161: An investigation of some aspects of the sonic boom by means of wind tunnel measurements of pressures about several bodies at mach number of 2.01 by Harry W. Carlson 44p
500			_aNASA TN D-162: Handbook of structural stability: Part VII strength of thin wing tunnel by George Gerard 83p
500			_aNASA TN D-163: Handbook of structural stability: Supplement to part III buckling of curved plates and shells23p
500			_aNASA TN D-164: A radar test target system by James T. Rose 53p
500			_aNASA TN D-165: A brief investigation of the effect of waves on the take off resistance of a seaplane by Elmo J. Mottard 17p
500			_aNASA TN D-166: A hydrodynamic investigation of the effect of adding upper surface camber to a submerged flat plate by Victor L. Vaughan 22p
500			_aNASA TN D-167: Investigation of variation in base pressure over the reynolds number range in which wake transition occurs for two dimensional bodies at mach numbers from 1.95 to 2.92 by Vernon Van Hise 44p
500			_aNASA TN D-168: Static force of several annular jet configurations in proximity to smooth and irregular ground by Edwin E. Davenport 13p
500			_aNASA TN D-169: Spectrographic temperature measurements in a carbon arc powered air jet by David H. Greenshields 24p
500			_aNASA TN D-170: Lift and drag charectristics at subsonic speeds and at a mach number of 1.9 of a lifting circular cylinder with a fineness ratio of 10 by Vernard E. Lockwood 21p
650			_aWind tunnel
942			_cTR
999			_c565872 _d565872