Lihat Juga

• ANALYSIS OF HYPERSONIC PRESSURE AND HEAT TRANSFER TESTS ON DELTA WINGS WITH LAMINAR AND TURBULENT BOUNDARY LAYERS
  oleh: NASA, WASHINGTON DC, AUGUST 1966
• CALCULATION OF COMPRESSIBLE TURBULENT BOUNDARY LAYERS WITH PRESSURE GRADIENTS AND HEAT TRANSFER
  oleh: NASA, WASHINGTON DC, MARCH 1969
• AN INVESTIGATION OF THE HIGH SPEED TURBULENT BOUNDARY LAYERS WITH HEAT TRANSFER AND ARBITRARY PRESSURE GRADIENT PART III
  oleh: NASA, WASHINGTON DC, OCTOBER 1970
• CALCULATION OF TURBULENT BOUNDARY LAYERS WITH HEAT TRANSFER AND PRESSURE GRADIENT UTILIZING A COMPRESSIBILITY TRANSFORMATION PART II
  oleh: NASA, WASHINGTON DC, JANUARY 1972
• CALCULATION OF TURBULENT BOUNDARY LAYERS WITH HEAT TRANSFER AND PRESSURE GRADIENT UTILIZING A COMPRESSIBILITY TRANSFORMATION PART I
  oleh: NASA, WASHINGTON DC, DECEMBER 1971