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22 catalog results

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1. Approximate method for calculation of laminar boundary layer with heat transfer on a cone at large angle of attack in supersonic flow [1958]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 4380

2. A comparison of two methods for calculating transient temperatures for thick walls [1958]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 4343

3. Approximate calculation of the compressible turbulent boundary layer with heat transfer and arbitrary pressure gradient [1957]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 4154

4. Experimental and calculated temperature and mass histories of vaporizing fuel drops [1956]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3490

5. Method of calculating core dimensions of crossflow heat exchanger with prescribed gas flows and inlet and exit states [1956]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3655

6. Some effects of bluntness on boundary-layer transition and heat transfer at supersonic speeds [1956]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3653

7. Analysis of fully developed turbulent heat transfer and flow in an annulus with various eccentricities [1955]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3451

8. Analysis of laminar forced-convection heat transfer in entrance region of flat rectangular ducts [1955]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3331

9. The compressible laminar boundary layer with heat transfer and arbitrary pressure gradient [1955]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3326

10. Free-flight measurements of turbulent-boundary-layer skin friction in the presence of severe aerodynamic heating at Mach numbers from 2.8 to 7.0 [1955]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3391

13. Method for calculation of compressible laminar boundary layer with axial pressure gradient and heat transfer [1954]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3157

14. Note on the aerodynamic heating of an oscillating surface [1954]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3146

15. A theoretical investigation of the heating-up period of injected fuel droplets vaporizing in air [1954]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3179

16. Transient temperatures in heat exchangers for supersonic blowdown tunnels [1954]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3078

17. Heat transfer and skin friction by an integral method in the compressible laminar boundary layer with a streamwise pressure gradient [1953]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3005

18. Investigation of laminar boundary layer in compressible fluids using the Crocco method [1952]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 2597

19. Laminar friction and heat transfer at Mach numbers from 1 to 10 [1951]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 2499

20. Analytical investigation of turbulent flow in smooth tubes with heat transfer with variable fluid properties for Prandtl number of 1 [1950]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 2242