WADC Technical ReportWright Air Development Division, Air Research and Development Command, United States Air Force, 1956 - Aeronautics |
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Common terms and phrases
6Al-4V Titanium Alloy aerodynamic aileron airfoil Aluminum angle of attack axis bearing creep Bearing Creep-Rupture Characteristics BEARING HOLE DIAMETER boundary layer Characteristics of PH15-7 coefficients Compression Creep contour CREEP DEFORMATION creep tests curve density displacement thickness distribution EDGE DISTANCE effects equations Figure finite fringe Flat Plate flow interferogram free-stream fuselage Hypersonic Inch inflection point isopycnic leading edge lift coefficient Loading Mach number measured Mo Stainless Steel Model N N N N N N N N N N N N N N N N N N N N N nozzle OL OL parameter PH15-7 Mo Stainless region RUPTURE shear Shear-Pin Deformation shock tube shock-tube Short-Time stagnation pressure Stainless Steel Sheet Static Pressure Ratio STRESS Supersonic surface Table 3 Continued TD C TD temperature tensile creep Tensile Creep-Rupture Characteristics test section TH 1050 CONDITION Titanium Alloy Bar Titanium Alloy Sheet ture Test two-dimensional unsteady values velocity viscous WADC TR wedge ო ო ო ო რ ო რ ო ო
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Page 34 - NOTICES When Government drawings, specifications, or other data are used for any purpose other than in connection with a definitely related Government procurement operation, the United States Government thereby incurs no responsibility nor any obligation whatsoever; and the fact that the Government may have formulated, furnished, or in any way supplied the said drawings, specifications, or other data, is not to be regarded by implication or otherwise as in any manner licensing the holder or any other...