NASA technical note [NASA TN D 161-170] 
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 .- Washington, D. C.: National Aeronautics and Space Administration,  1959 
.- ( National Aeronautics and Space Administration NASA Technical note   
<br/>NASA 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 NASA TN D-162: Handbook of structural stability: Part VII strength of thin wing tunnel by George Gerard 83p NASA TN D-163: Handbook of structural stability: Supplement to part III buckling of curved plates and shells23p NASA TN D-164: A radar test target system by James T. Rose 53p NASA TN D-165: A brief investigation of the effect of waves on the take off resistance of a seaplane by Elmo J. Mottard 17p NASA TN D-166: A hydrodynamic investigation of the effect of adding upper surface camber to a submerged flat plate by Victor L. Vaughan 22p NASA 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 NASA TN D-168: Static force of several annular jet configurations in proximity to smooth and irregular ground by Edwin E. Davenport 13p NASA TN D-169: Spectrographic temperature measurements in a carbon arc powered air jet by David H. Greenshields 24p NASA 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 
<br/><u>Subject Headings:</u> <br/>Wind tunnel;
<br><U>Copy Details:</u><br> Acc. No.: <b>63641</b>, Full Call No.: ,   Item type:  Technical Report , Location: COMPACT STORAGE (BASEMENT), NASA TN D 161-170<br><b>------------------------- --------------------- ------ --------- ------- ------- --------- -------- </b><br>