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FREECONVECTION BOUNDARYLAYER SOLUTIONS 13
CONCLUDING REMARKS 20
3 other sections not shown
aerodynamic Aeronautics and Space ailerons aircraft airloads altitude angle of attack blade boundary layer boundary-layer flows buffeting calculated coatings computed corrosion damper deflection dimensionless disk drag rise effect equation exact solutions experimental finite difference solution flat plate flight flow free convection friction and wear gases harmonic Hastelloy heat transfer heat-transfer results Inconel investigation isothermal vertical plate jet transports Langley Field load low Prandtl number lubrication M-l tool steel Mach number maneuver measured method METHONS NACA NACA RM NACA TN NASA National Aeronautics NSAA MEME obtained oxide percent SFg Prandtl number range presented reference region rotation rotor shear stress shock wave shown in figure Simpson's rule sonic line Space Administration Stellite stream function structural moments subsonic supersonic surface take-off test airplane thermal tion TRANSPORT CONFIGURATIONS tropopause u-ME uniform wall temperature upstream transpiration cooling variable wing YSAA MEMERAN,M