NASA technical note [NASA TN 2971-2980]
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.- Washington, D. C.: National Aeronautics and Space Administration, 1953
.- ( National Aeronautics and Space Administration NASA Technical Report
NASA TN 2971: Impingement of water droplets on wedges and diamond airfoils at supersonic speeds by John S. Serafini 62p NASA TN 2972: Theoretical pressure distributions and wave drags for conical bottalls by John R. Jack 14p NASA TN 2973: Effect of prestraining on recrystallization temperature and mechanical properties of commercial sintered brought molybdenum by Kenneth C. Dike 25p NASA 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 NASA TN 2975: Structural efficiences of various aluminium titanium and steel alloys at elevated temperatures by George J. Heimerl 16p NASA TN 2976: A study of the stability of the incompressible laminar boundary layer on infinite wedges by Neal Tetervin 41p NASA TN 2977: Techniques for calculating parameters of nonlinear dynamic systems from response data by Benjamin R. Briggs 65p NASA 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 NASA 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 NASA 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
Subject Headings:
Boundary layer;
Copy Details:
Acc. No.: 67649, Full Call No.: , Item type: Technical Report , Location: COMPACT STORAGE (BASEMENT), NASA TN 2971-2980
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NASA TN 2971: Impingement of water droplets on wedges and diamond airfoils at supersonic speeds by John S. Serafini 62p NASA TN 2972: Theoretical pressure distributions and wave drags for conical bottalls by John R. Jack 14p NASA TN 2973: Effect of prestraining on recrystallization temperature and mechanical properties of commercial sintered brought molybdenum by Kenneth C. Dike 25p NASA 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 NASA TN 2975: Structural efficiences of various aluminium titanium and steel alloys at elevated temperatures by George J. Heimerl 16p NASA TN 2976: A study of the stability of the incompressible laminar boundary layer on infinite wedges by Neal Tetervin 41p NASA TN 2977: Techniques for calculating parameters of nonlinear dynamic systems from response data by Benjamin R. Briggs 65p NASA 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 NASA 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 NASA 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
Subject Headings:
Boundary layer;
Copy Details:
Acc. No.: 67649, Full Call No.: , Item type: Technical Report , Location: COMPACT STORAGE (BASEMENT), NASA TN 2971-2980
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