Author: Richard J. McCafferty
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 44
Book Description
Analytical Investigation of Fuel Temperatures and Fuel-evaporation Losses Encountered in Long-range High-altitude Supersonic Flight
Author: Richard J. McCafferty
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 44
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 44
Book Description
Generalized Tables of Corrections to Thermodynamic Properties for Nonpolar Gases
Author: Harold William Woolley
Publisher:
ISBN:
Category : Gas
Languages : en
Pages : 670
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.
Publisher:
ISBN:
Category : Gas
Languages : en
Pages : 670
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.
Technical Note
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 654
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 654
Book Description
Technical Note - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1224
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1224
Book Description
Analytical Heat Transfer Investigation of Insulated Liquid Methane Fuselage Tanks for Supersonic Cruise Aircraft
Author: Eugene J. Pleban
Publisher:
ISBN:
Category : Fuel
Languages : en
Pages : 20
Book Description
Publisher:
ISBN:
Category : Fuel
Languages : en
Pages : 20
Book Description
Catalog of Books and Reports in the Bureau of Mines Technical Library, Pittsburgh, Pa
Author: United States. Bureau of Mines. Technical Library, Pittsburgh
Publisher:
ISBN:
Category : Library catalogs
Languages : en
Pages : 522
Book Description
Publisher:
ISBN:
Category : Library catalogs
Languages : en
Pages : 522
Book Description
Annual Report of the National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 90
Book Description
Includes the Committee's Reports no. 1-1058, reprinted in v. 1-37.
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 90
Book Description
Includes the Committee's Reports no. 1-1058, reprinted in v. 1-37.
Report
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 524
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 524
Book Description
Analytical Heat Transfer Investigation of Insulated Liquid Methane Wing Tanks for Supersonic Cruise Aircraft
Author: Eugene J. Pleban
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 44
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).
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 44
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).
Annual Report
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 534
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 534
Book Description