Books by Harold Mirels:
Books in the extended shelves:
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Mirels, Harold: Analysis of one-dimensional ion rocket with grid neutralization (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 (U.S. G.P.O.], 1959) (page images at HathiTrust)
- Mirels, Harold: Axisymmetric hypersonic flow with strong viscous interaction (Los Angeles, California : Space Systems and Ballistic Systems Divisions, Los Angeles Air Force Station, Air Force Systems Command, United States Air Force, 1967., 1967), also by John Webster Ellinwood, United States. Air Force. Systems Command. Space Systems Division, and Aerospace Corporation (page images at HathiTrust)
- Mirels, Harold: Effect of body perturbations on hypersonic flow over slender power law bodies (U.S. G.P.O.], 1959) (page images at HathiTrust)
- Mirels, Harold: Expansion of gas clouds and hypersonic jets bounded by a vacuum. (Aerospace Corp., 1962), also by James Francis Mullen and Aerospace Corporation (page images at HathiTrust)
- Mirels, Harold: Laminar boundary layer behind a strong shock moving into air (National Aeronautics and Space Administration, 1960) (page images at HathiTrust; US access only)
- Mirels, Harold: Line-vortex theory for calculation of supersonic downwash (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. (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 (Los Angeles, California : Space and Missile Systems Organization, Los Angeles Air Force Station, Air Force Systems Command, United States Air Force, 1967., 1967), also by William E Welsh, United States. Air Force. Systems Command, Space and Missile Systems Organization (U.S.), and Aerospace Corporation (page images at HathiTrust)
- Mirels, Harold: Subsonic flow of hot gas through a highly cooled constant-area channel (Los Angeles, California : Space and Missile Systems Organization, Los Angeles Air Force Station, Air Force Systems Command, United States Air Force, 1967., 1967), also by United States. Air Force. Systems Command, Space and Missile Systems Organization (U.S.), and 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 (National Aeronautics and Space Administration :, 1961), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
- Mirels, Harold: Wing tip with subsonic trailing edge (National Advisory Committee for Aeronautics, 1949), also by James M. Jagger and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
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