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21. Two-dimensional diffusion theory analysis of reactivity effects of a fuel-plate-removal experiment [1958]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 4164

22. Use of the kernel function in a three-dimensional flutter analysis with application to a flutter-tested delta-wing model [1958]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 4395

23. 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

24. Characteristics of a 40 degree cone for measuring Mach number, total pressure, and flow angles at supersonic speeds [1957]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3967

25. Comparison of calculated and experimental load distributions on thin wings at high subsonic and sonic speeds [1957]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3941

26. Drop-size distribution for crosscurrent breakup of liquid jets in airstreams [1957]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 4087

27. Estimation of compressible boundary-layer growth over insulated surfaces with pressure gradient [1957]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 4022

28. Estimation of incremental pitching moments due to trailing-edge flaps on swept and triangular wings [1957]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 4040

29. A general system for calculating burning rates of particles and drops and comparison of calculated rates for carbon, boron, magnesium, and isooctane [1957]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3929

30. Lift and moment responses to penetration of sharp-edged traveling gusts, with application to penetration of weak blast waves [1957]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3956

31. On the minimization of airplane responses to random gusts [1957]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3290

32. Nonuniformities in shock-tube flow due to unsteady-boundary-layer action [1957]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 4021

33. Theoretical calculations of supersonic wave drag at zero lift for a particular store arrangement [1957]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 4120

35. Theory of self-excited mechanical oscillations of helicopter rotors with hinged blades [1957]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3844

36. Aerodynamic interference of slender wing-tail combinations [1956]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3725

37. Analytical determination of the natural coupled frequencies and mode shapes and the response to oscillating forcing functions of tandem helicopters [1956]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3849

38. Calculation and compilation of the unsteady-lift functions for a rigid wing subjected to sinusoidal gusts and to sinusoidal sinking oscillations [1956]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3748

39. Calculation of the forces and moments on a slender fuselage and vertical fin penetrating lateral gusts [1956]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3805

40. Comparison of several methods for obtaining the time response of linear systems to either a unit impulse or arbitrary input from frequency-response data [1956]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3701