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1. Analytical and experimental investigation of aerodynamic forces and moments on low-aspect-ratio wings undergoing flapping oscillations [1958]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 4302

3. An approximate analytical method for studying entry into planetary atmospheres [1958]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 4276

4. 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

5. 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

6. Effect of angle of attack and thickness on aerodynamic coefficients of a rigid wing oscllating at very low frequencies in two-dimensional supersonic flow [1958]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 4069

7. Flow induced by a rotor in power-on vertical descent [1958]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 4330

8. Flutter analysis of rectangular wings of very low aspect ratio [1958]

  • SAL3 (off-campus storage) : Stacks : NACA TN 4245

10. A numerical method for evaluating wave drag [1958]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 4258

12. On pairs of solutions of a class of internal viscous flow problems with body forces [1958]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 4273

13. Procedure for calculating flutter at high supersonic speed including camber deflections, and comparisons with experimental results [1958]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 4335

14. Relative motion in the terminal phase of interception of a satellite or a ballistic missile [1958]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 4399

15. On solutions for the transient response of beams [1958]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 4244

16. Statistical study of turbulence : spectral functions and correlation coefficients [1958]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TM 1436

18. Temperature and thermal-stress distributions in some structural elements heated at a constant rate [1958]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 4306

19. Theoretical investigation of subsonic oscillatory blade-row aerodynamics [1958]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 4136

20. Theoretical pressure distributions for several related nonlifting airfoils at high subsonic speeds [1958]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 4148

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

41. Effect of transverse body force on channel flow with small heat addition [1956]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3594

42. Equations and procedures for numerically calculating the aerodynamic characteristics of lifting rotors [1956]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3747

43. 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

45. Lift and moment coefficients for an oscillating rectangular wing-aileron configuration in supersonic flow [1956]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3644

47. Method for calculating the aerodynamic loading on an oscillating finite wing in subsonic and sonic flow [1956]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3694

48. A method for calculating the contour of bodies of revolution with a prescribed pressure gradient at supersonic speed with experimental verification [1956]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3555

49. A method for calculation of free-space sound pressures near a propeller in flight including considerations of the chordwise blade loading [1956]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3809

50. A method for deflection analysis of thin low-aspect-ratio wings [1956]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3640

51. 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

52. Minimum-drag ducted and closed three-point body of revolution based on linearized supersonic theory [1956]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3704

53. Normal component of induced velocity in the vicinity of a lifting rotor with a nonuniform disk loading [1956]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3690

54. An optimum switching criterion for a third-order contactor acceleration control system [1956]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3743

55. Particular solutions for flows at Mach number 1 [1956]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3868

56. Poisson's ratios and volume changes for plastically orthotropic material [1956]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3736

57. On possible similarity solutions for three-dimensional incompressible laminar boundary layers. 2, Similarity with respect to stationary polar coordinates [1956]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3832

58. Preliminary investigation of a family of diffusers designed for near sonic inlet velocities [1956]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3668

59. On the range of applicability of the transonic area rule [1956]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3673

60. A relation between burning velocity and quenching distance [1956]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3882

61. A simple method for calculating the characteristics of the dutch roll motion of an airplane [1956]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3754

62. 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

63. Stability derivatives of cones at supersonic speeds [1956]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3788

64. Theoretical analysis of linked leading-edge and trailing-edge flap-type controls at supersonic speeds [1956]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3617

65. Theoretical loss relations for low-speed two-dimensional-cascade flow [1956]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3662

66. Three-dimensional transonic flow theory applied to slender wings and bodies [1956]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3717

67. An accurate and rapid method for the design of supersonic nozzles [1955]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3322

68. Analysis of errors introduced by several methods of weighting nonuniform duct flows [1955]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3400

69. 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

70. 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

72. Analysis of two-dimensional compressible-flow loss characteristics downstream of turbomachine blade rows in terms of basic boundary-layer characteristics [1955]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3515

73. Analytic determination of the discharge coefficients of flow nozzles [1955]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3447

74. An approximate solution for axially symmetric flow over a cone with an attached shock wave [1955]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3485

75. Calculated spanwise lift distributions and aerodynamic influence coefficients for swept wings in subsonic flow [1955]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3476

76. On the calculation of the 1-P oscillating aerodynamic loads on single-rotation propellers in pitch on tractor airplanes [1955]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3395

77. 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

78. Correction of additional span loadings computed by the Weissinger seven-point method for moderately tapered wings of high aspect ratio [1955]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3500

79. An experimental comparison of the Lagrangian and Eulerian correlation coefficients in homogeneous isotropic turbulence [1955]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3570

80. 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

82. The linearized equations of motion underlying the dynamic stability of aircraft, spinning projectiles, and symmetrical missiles [1955]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3350

83. A method for studying the transient blade-flapping behavior of lifting rotors at extreme operating conditions [1955]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3366

84. One-dimensional calculation of flow in a rotating passage with ejection through a porous wall [1955]

  • SAL3 (off-campus storage) : Stacks : NACA TN 3408

85. Practical considerations in specific applications of gas-flow interferometry [1955]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3507

86. A rapid approximate method for the design of hub shroud profiles of centrifugal impellers of given blade shape [1955]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3399

88. Second-order subsonic airfoil-section theory and its practical application [1955]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3390

89. On slender delta wings with leading-edge separation [1955]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3430

92. Theoretical span load distributions and rolling moments for sideslipping wings of arbitrary plan form in incompressible flow [1955]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3605

93. Total lift and pitching moment of thin arrowhead wings oscillating in supersonic potential flow [1955]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3433

94. A wind-tunnel test technique for measuring the dynamic rotary stability derivatives including the cross derivatives at high Mach numbers [1955]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3347

95. Aerodynamic forces, moments, and stability derivatives for slender bodies of general cross section [1954]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3283

96. Aerodynamic investigation of a four-blade propeller operating through an angle-of-attack range from 0 to 180 degrees [1954]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3228

97. Analog study of interacting and noninteracting multiple-loop control systems for turbojet engines [1954]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3112

98. An analysis of shock-wave cancellation and reflection for porous walls which obey and exponential mass-flow pressure-difference relation [1954]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3223

99. Application of two-dimensional vortex theory to the prediction of flow fields behind wings of wing-body combinations at subsonic and supersonic speeds [1954]

  • SAL3 (off-campus storage) : See linked record to request items bound together : NACA TN 3227