Author : George R. Costello
Publisher :
Page : 32 pages
File Size : 35,37 MB
Release : 1949
Category : Aerofoils
ISBN :
By the assumption that the pressure-volume relation is linear, a method is given for computing the airfoil shape with a prescribed velocity distribution in a potential flow of a compressible nonviscous fluid.
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 1026 pages
File Size : 24,1 MB
Release : 1956
Category : Aeronautics
ISBN :
Author : Lewis Research Center
Publisher :
Page : 542 pages
File Size : 43,3 MB
Release : 1965
Category : Axial flow compressors
ISBN :
Author : Robert O. Bullock
Publisher :
Page : 552 pages
File Size : 47,46 MB
Release : 1965
Category : Axial flow compressors
ISBN :
Author : John R. Spreiter
Publisher :
Page : 646 pages
File Size : 41,50 MB
Release : 1949
Category : Aerodynamic load
ISBN :
The aerodynamic forces and moments exerted on pitched and yawed wing-body combinations consisting of a slender body of revolution and a cruciform arrangement of thin wings have been investigated by two theoretical methods. One method, an extension of the slender wing-body theory of NACA TN No. 1662, makes possible the determination of simple closed expressions for the load distribution, of simple closed expressions for the load distribution, the forces, and the moments for slender cruciform-wing and body combinations in which the wings may be dissimilar plan form. The second method treats cruciform-wing and body combinations consisting of a body of revolution and identical wings of arbitrary aspect ratio and plan form. The results are valid at subsonic, transonic, and supersonic speeds.
Author :
Publisher :
Page : 568 pages
File Size : 49,57 MB
Release : 1972
Category : Mechanics, Applied
ISBN :
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 498 pages
File Size : 27,63 MB
Release : 1952
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 750 pages
File Size : 36,4 MB
Release : 1949
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 488 pages
File Size : 45,49 MB
Release : 1958
Category : Aerodynamics
ISBN :
Author : Alois T. Sutor
Publisher :
Page : 706 pages
File Size : 21,22 MB
Release : 1951
Category : Airplanes
ISBN :
Analytical expressions are derived to show the geometric, thermodynamic, and aerodynamic relations among compressor, turbine, and exhaust nozzle for a gas-turbine engine. For a known compressor performance map, a matching method is described to show some of the design compromises that must be made when the components are to be combined into a turbine-propeller engine. A method of predicting engine performance for a range of operating conditions from known component maps is presented. An illustrative example of the matching method and the performance analysis is presented, showing some of the practical limitations of engine operation.
