Effect of Heat and Power Extraction on Turbojet-engine Performance IV
Author : Stanley L. Koutz
Publisher :
Page : pages
File Size : 16,16 MB
Release : 1951
Category :
ISBN :
Effect of Heat and Power Extraction on Turbojet-engine Performance
Author : Stanley L. Koutz
Publisher :
Page : 52 pages
File Size : 17,97 MB
Release : 1951
Category : Airplanes
ISBN :
Book Description
In general, with a turbojet engine operating at constant engine speed, bleeding gas from the tail pipe at constant tail-pipe-nozzle area and reduced turbine-inlet temperature caused 2.5 to 4 times as great a loss in thrust as bleeding gas at constant turbine-inlet temperature and reduced tail-pipe-nozzle area.
Effect of Heat and Power Extraction on Turbojet-engine Performance
Author : Frank E. Rom
Publisher :
Page : 18 pages
File Size : 36,58 MB
Release : 1950
Category : Airplanes
ISBN :
Book Description
The effect of compressor-outlet air bleed on the performance of an axial-flow turbojet engine is presented.
Effect of Heat and Power Extraction on Turbojet-engine Performance
Author : Stanley L. Koutz
Publisher :
Page : 49 pages
File Size : 23,22 MB
Release : 1950
Category : Airplanes
ISBN :
Book Description
Generalized working charts, prepared by matching experimentally determined component characteristics of a typical axial-flow-type turbojet engine, are presented for determining the effect of shaft-power extraction on engine performance.
Turbulent Boundary-layer Temperature Recovery Factors in Two-dimensional Supersonic Flow
Author : Maurice Tucker
Publisher :
Page : 686 pages
File Size : 47,48 MB
Release : 1951
Category : Aerodynamics, Supersonic
ISBN :
Book Description
An analytical method is presented for obtaining turbulent temperature recovery factors for a thermally insulated surface in supersonic flow. The method is an extension of Squire's analysis for incompressible flow. The boundary layer velocity profile is represented by a power law and a similarity is postulated for squared-velocity the static-temperature-difference profiles.
Technical Note - National Advisory Committee for Aeronautics
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 434 pages
File Size : 23,44 MB
Release : 1950
Category : Aeronautics
ISBN :
Book Description
Technical Note - National Advisory Committee for Aeronautics
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 700 pages
File Size : 43,42 MB
Release : 1951
Category : Aeronautics
ISBN :
Book Description
Investigation of a Full-scale, Cascade-type Thrust Reverser
Author : Robert C. Kohl
Publisher :
Page : 728 pages
File Size : 41,2 MB
Release : 1957
Category : Cascades (Fluid dynamics)
ISBN :
Book Description
A double set of turning vanes was carried inside the jet tailpipe. To produce reverse thrust, the tailpipe opens into two side sections and the turning vanes move outward to form a V-shaped cascade, which deflects the exhaust-gas flow. Forward and reverse net thrust were measured over a range of engine speeds with the airplane stationary. Taxi tests were made to determine the comparative stopping distances using wheel braking and reverse thrust separately, and a combination of both. The effect of turning-vane spacing on thrust-reverser performance was determined by scale-model tests using unheated air.
Monthly Catalog of United States Government Publications
Author :
Publisher :
Page : 1444 pages
File Size : 19,33 MB
Release : 1951
Category : Government publications
ISBN :
Book Description
Index of NACA Technical Publications
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 242 pages
File Size : 24,89 MB
Release : 1955
Category : Aeronautics
ISBN :
