The Online Books Page

Online Books by

Harold Mirels

Books from the extended shelves:

• Mirels, Harold: Analysis of one-dimensional ion rocket with grid neutralization / (Washington, [D.C.] : National Aeronautics and Space Administration, 1960), also by Burt M. Rosenbaum and Lewis Research Center (page images at HathiTrust)
• Mirels, Harold: Approximate analytical solutions for hypersonic flow over slender power law bodies, ([Washington, U.S. G.P.O.], 1959) (page images at HathiTrust)
• Mirels, Harold: Axisymmetric hypersonic flow with strong viscous interaction /, also by John Webster Ellinwood, issuing body United States. Air Force. Systems Command. Space Systems Division, and sponsor Aerospace Corporation (page images at HathiTrust)
• Mirels, Harold: Effect of body perturbations on hypersonic flow over slender power law bodies, ([Washington, U.S. G.P.O.], 1959) (page images at HathiTrust)
• Mirels, Harold: Expansion of gas clouds and hypersonic jets bounded by a vacuum. (El Segundo, Calif., Aerospace Corp., 1962), also by James Francis Mullen and Aerospace Corporation (page images at HathiTrust)
• Mirels, Harold: Experimental pressure distributions over wing tips at Mach number 1.9. (Washington, D.C. : National Advisory Committee for Aeronautics, [1949]), also by James M. Jagger, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Mirels, Harold: Laminar boundary layer behind a strong shock moving into air / (Washington, DC : National Aeronautics and Space Administration, 1960) (page images at HathiTrust; US access only)
• Mirels, Harold: Line-vortex theory for calculation of supersonic downwash / (Washington, D.C. : National Advisory Committee for Aeronautics, 1949), also by Rudolph C. Haefeli and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Mirels, Harold: Shock-bounded, self-similar flows with volumetric mass, momentum, and energy addition. (El Segundo, Calif., Aerospace Corp., 1962), also by Mullen James Francis and Aerospace Corporation (page images at HathiTrust)
• Mirels, Harold: Shock tube test time limitation due to turbulent wall boundary layer. ([El Segundo?], 1963), also by Aerospace Corporation (page images at HathiTrust)
• Mirels, Harold: Stagnation point boundary layer with large wall-to-freestream enthalpy ratio /, also by William E Welsh, issuing body United States. Air Force. Systems Command, sponsor Space and Missile Systems Organization (U.S.), and sponsor Aerospace Corporation (page images at HathiTrust)
• Mirels, Harold: Subsonic flow of hot gas through a highly cooled constant-area channel /, also by issuing body United States. Air Force. Systems Command, sponsor Space and Missile Systems Organization (U.S.), and sponsor Aerospace Corporation (page images at HathiTrust)
• Mirels, Harold: Test time in low pressure shock tubes. (El Segundo?], 1962), also by Aerospace Corporation (page images at HathiTrust)
• Mirels, Harold: Two-dimensional ion beams with small lateral spreading / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1961]), also by United States National Aeronautics and Space Administration (page images at HathiTrust)

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