Results 131 to 140 of about 3,568 (253)
Surge margin monitoring of one turboshaft engine with inlet distortion [PDF]
Siqi Yan +3 more
openalex +1 more source
General Aviation Turbine Engine (GATE) study [PDF]
The feasibility of turbine engines for the smaller general aviation aircraft was investigated and a technology program for developing the necessary technology was identified.
Baerst, C. F., Furst, D. G.
core +1 more source
A simplified dynamic model of the T700 turboshaft engine [PDF]
A simplified open-loop dynamic model of the T700 turboshaft engine, valid within the normal operating range of the engine, is developed. This model is obtained by linking linear state space models obtained at different engine operating points.
Duyar, Ahmet +2 more
core +1 more source
Helicopters Turboshaft Engines Neural Network Modeling under Sensor Failure [PDF]
Serhii Vladov +4 more
openalex +1 more source
Modeling of A Miso Control System For A Turboshaft Engine [PDF]
Arkan Altaie, Usama S.Salah
openalex +1 more source
Preliminary study of advanced turboprop and turboshaft engines for light aircraft [PDF]
The effects of engine configuration, advanced component technology, compressor pressure ratio and turbine rotor-inlet temperature on such figures of merit as vehicle gross weight, mission fuel, aircraft acquisition cost, operating, cost and life cycle ...
Eisenberg, J. D. +2 more
core +1 more source
VASCOMP 2. The V/STOL aircraft sizing and performance computer program. Volume 6: User's manual, revision 3 [PDF]
This report describes the use of the V/STOL Aircraft Sizing and Performance Computer Program (VASCOMP II). The program is useful in performing aircraft parametric studies in a quick and cost efficient manner. Problem formulation and data development were
Rosenstein, H. +3 more
core +1 more source
Threats from and Countermeasures for Unmanned Aerial and Underwater Vehicles. [PDF]
Khawaja W +5 more
europepmc +1 more source
The influence of engine/transmission/governor on tilting proprotor aircraft dynamics [PDF]
An analytical model is developed for the dynamics of a tilting proprotor aircraft engine and drive train, including a rotor speed governor and interconnect shaft.
Johnson, W.
core +1 more source

