Author : Ralph T. Dittrich
Publisher :
Page : 34 pages
File Size : 32,18 MB
Release : 1948
Category : Carbon
ISBN :
A study was made to determine the cause of irreproducibility of combustion data of a single tubular-type turbojet combustor operating at simulated altitude conditions.
Author :
Publisher :
Page : 388 pages
File Size : 42,34 MB
Release : 1948
Category : Aeronautics
ISBN :
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 774 pages
File Size : 31,35 MB
Release : 1948
Category : Aeronautics
ISBN :
Author : Jerrold D. Wear
Publisher :
Page : 20 pages
File Size : 49,52 MB
Release : 1951
Category : Aeronautics
ISBN :
Author : Edward G. Stricker
Publisher :
Page : 28 pages
File Size : 11,56 MB
Release : 1950
Category : Aeronautics
ISBN :
The combustion efficiency and the altitude operational limits of three liquid hydrocarbon fuels having high volumetric energy content (decalin, tetralin, and monomethylnaphthalene) were compared with an AN-F-58 fuel in a single tubular combustor from a J33 turbojet engine. The investigation covered a range of simulated engine conditions for altitudes from 20,000 to 60,000 feet; 42- to 107-percent normal rated engine speed; and a flight Mach number of 0.6. The independent effects of combustor-inlet-air temperature, pressure, and mass air flow on the combustion efficiency of the fuels were determined around a standard combustion-inlet condition.
Author :
Publisher :
Page : 90 pages
File Size : 42,96 MB
Release : 1950
Category : Aeronautics
ISBN :
Author : Warren A. Tucker
Publisher :
Page : 738 pages
File Size : 12,46 MB
Release : 1948
Category : Aerodynamics, Supersonic
ISBN :
A theoretical analysis, based on the linearized equation for supersonic flow, of characteristics of triangular-tip control surfaces on thin triangular wings. By restriction to case for which Mach lines from wing apex lie behind the leading edge, a simplified treatment was possible; results of previous work on lift of triangular wings could be used to derive expressions for lift effectiveness, pitching moment, rolling-moment effectiveness, hinge moment due to control deflection, and hinge moment due to angle of attack. Comparisons were made with two-dimensional case.
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 666 pages
File Size : 50,52 MB
Release : 1951
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 1620 pages
File Size : 42,17 MB
Release : 1948
Category : Government publications
ISBN :
Author : North Atlantic Treaty Organization. Advisory Group for Aeronautical Research and Development
Publisher :
Page : 542 pages
File Size : 27,28 MB
Release : 1956
Category : Combustion
ISBN :
