Results 111 to 120 of about 19,118 (298)

Experimental investigation of cermet turbine blades in an axial-flow turbojet engine [PDF]

, 1958
William C. Morgan, G. C. Deutsch
openalex   +1 more source

Calculus Of Turbojet Performances For Ideal Case

, 2014
{"references": ["A. H. Lefebvre and D. R. Ballal, Gas Turbines Combustion, 3rd ed. Taylor & Francis, New York, 2010.", "J. C. Han, S. Dutta and S. Ekkad, Gas Turbine Heat Transfer and Cooling Technology. Taylor & Francis, New York, 2000.", "F. Liu and W. A. Sirignano, \"Turbojet and Turbofan Engine Performance Increases through Turbine Burners\"
S. Bennoud, S. Hocine, H. Slme
openaire   +1 more source

Advanced exergy analysis of a turbojet engine main components considering mexogenous, endogenous, exegenous, avoidable and unavoidable exergy destructions

Propulsion and Power Research, 2022
H. Caliskan, S. Ekici, Yasin Sohret
semanticscholar   +1 more source

Turbojet and turbofan engines for a mach 3 supersonic transport [PDF]

, 1964
James Dugan, R. W. Koenig, T. B. Mc Auliffe, J. B. Whitlow   +3 more
openalex   +1 more source

NACA Investigations of Icing-Protection Systems for Turbojet-Engine Installations [PDF]

Investigations have been made in flight and in wind tunnels to determine which components of turbojet installations are most critical in icing conditions, and to evaluate several methods of icing protection. From these studies, the requirements necessary
Callaghan, Edmund E., Gray, Vernon H., VonGlahn, Uwe   +2 more
core   +1 more source

Noise Levels of Turbojet- and Turbofan-Powered Aircraft [PDF]

, 1962
Alan H. Marsh, A. L. McPike
openalex   +1 more source

POSSIBLE APPVOACH TO COMPUTATIONAL AND ANALYTICAL CALCULATION OF THE STRESS INTENSITY FACTOR FOR THE BLADE OF THE TURBOJET

Научный вестник МГТУ ГА, 2016
This paper covers one stress intensity factor calculation method for the blades of the turbojet.
A. E. Sheryshev, D. V. Telnov
doaj  

Quantitative and stability study of the evolution of a thermoelastic body. [PDF]

MethodsX, 2023
Zinsou PH, Degla G, Ezzinbi K.
europepmc   +1 more source

Identification and dual adaptive control of a turbojet engine [PDF]

The objective of this paper is to utilize the design methods of modern control theory to realize a dual-adaptive feedback control unit for a highly nonlinear single spool airbreathing turbojet engine.
Leininger, G., Merrill, W.
core   +1 more source

Photographic data on the influence of the composition, preparation method, time and fuel system on the size of water droplets in a fuel-water emulsion. [PDF]

Data Brief, 2022
Niszczota P, Gieras M.
europepmc   +1 more source