Analytical Investigation of Fuel Temperatures and Fuel-evaporation Losses Encountered in Long-range High-altitude Supersonic Flight PDF Download
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Author: Richard J. McCafferty
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 44
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Book Description
Author: Richard J. McCafferty
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 44
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Book Description
Author: Harold William Woolley
Publisher:
ISBN:
Category : Gas
Languages : en
Pages : 670
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Book Description
Tables are presented based on the Lennard-Jones 6-12 potential for nonpolar molecules to be used in the representation of second and third virial coefficients and equation-of-state corrections for enthalpy, entropy, specific heats at constant volume and at constant pressure, the ratio of specific heats, the isentropic expansion coefficient, and the velocity of sound. The treatment for effects involving three molecules jointly uses an empirical adjustment of the Lennard-Jones force parameters within a cluster of three independently of the value for an isolated pair. A graphical correlation of ratios of these parameters with the critical constants is also shown which permits better estimates for compact nonpolar molecules with known critical constants but with limited data of state.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1224
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 654
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Book Description
Author: Eugene J. Pleban
Publisher:
ISBN:
Category : Fuel
Languages : en
Pages : 20
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Book Description
Author: United States. Bureau of Mines. Technical Library, Pittsburgh
Publisher:
ISBN:
Category : Library catalogs
Languages : en
Pages : 522
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Author: Eugene J. Pleban
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 44
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Book Description
Liquid methane boiloff from wing tanks was computed for typical SST missions for cruise Mach numbers of 2.7, 3.0, 3. 5, insulation thicknesses varying from 0. 5 to 2 in. (1.27 to 5.08 cm), various vent pressure settings, and saturated and subcooled fuel. Boiloff rates during fuel fill and ground hold are discussed. Boiloff losses less than 121 percent are possible for cruise Mach numbers up to 3. 5 for an insulation thickness of 1 in. (2.54 cm).
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 524
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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 90
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Book Description
Includes the Committee's Reports no. 1-1058, reprinted in v. 1-37.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 534
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Book Description
