000			02136nam a22003017a 4500
003			OSt
005			20220722145002.0
008			220722b xxu||||| |||| 00| 0 eng d
040			_cIIT Kanpur
041			_aeng
110			_aWashington: National Aeronautics and Space Administration
245			_aNASA technical note [NASA TN 2971-2980]
260			_aWashington, D. C. _bNational Aeronautics and Space Administration _c1953
440			_aNational Aeronautics and Space Administration
440			_aNASA Technical Report
500			_aNASA TN 2971: Impingement of water droplets on wedges and diamond airfoils at supersonic speeds by John S. Serafini 62p
500			_aNASA TN 2972: Theoretical pressure distributions and wave drags for conical bottalls by John R. Jack 14p
500			_aNASA TN 2973: Effect of prestraining on recrystallization temperature and mechanical properties of commercial sintered brought molybdenum by Kenneth C. Dike 25p
500			_aNASA TN 2974: Experiments on mixed free and forced convective heat transfer connected with turbulent flow through a short tube by E. R. G. Eckert 59p
500			_aNASA TN 2975: Structural efficiences of various aluminium titanium and steel alloys at elevated temperatures by George J. Heimerl 16p
500			_aNASA TN 2976: A study of the stability of the incompressible laminar boundary layer on infinite wedges by Neal Tetervin 41p
500			_aNASA TN 2977: Techniques for calculating parameters of nonlinear dynamic systems from response data by Benjamin R. Briggs 65p
500			_aNASA TN 2978: An approximate method of calculating the deformations of wing having swept M or W, A, and swept-tip plan forms by George W. Zender 28p
500			_aNASA TN 2979: Effects of symmetric and asymmetric thrust reversal on the aerodynamic characteristics of a model of a twin engine airplane by Kenneth W. Goodson 67p
500			_aNASA TN 2980: The aerodynamic characteristics of an aspect ratio 20 wing having thick airfoil sections and employing boundary layer control by suction by Bennie W. Cocke 63p
650			_aBoundary layer
942			_cTR
999			_c565934 _d565934