Journal of Aerospace Technology and Management, 2011 The main objective of this work was to present the specifi cation of an experimental fi ring test stand for liquid rocket engines (LRE) and develop a program for control and acquisition of data.
Emerson Andrade Santos +3 more
doaj
A comparison of the three methods used to obtain acoustic measurements for the NASA Flight Effects Program [PDF]
The NASA Flight Effects Program has a requirement to compare acoustic data obtained from flyover, static test stand, and wind tunnel tests. Results a laboratory study of the acoustic characteristics of the three technqiues used to measure noise during ...
Mueller, A. W.
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Parametric tests of a traction drive retrofitted to an automotive gas turbine [PDF]
The results of a test program to retrofit a high performance fixed ratio Nasvytis Multiroller Traction Drive in place of a helical gear set to a gas turbine engine are presented.
Anderson, N. E. +2 more
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STAND FOR TEST HYDRAULIC MACHINES WITH RECUPERATION OF THE ENERGY
Advanced Engineering Research, 2009 The principle scheme of the stand is оffered for test the hydraulic machines with economy of the energy. Happens to its mathematical model and information about its preliminary analysis.
A.T. RYBAK, A.V. SERDYUKOV
doaj
PC8B-4-X562 fuel cell electrical power supply, operations manual [PDF]
The PC8B-4 fuel cell electrical power supply is an electrical powerplant designed to convert the chemical reaction of hydrogen and oxygen into electrical energy. It utilizes catalyzed electrodes with a potassium hydroxide electrolyte.
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STAND FOR TEST HYDRAULIC MACHINES WITH RECUPERATION OF THE ENERGY
Вестник Донского государственного технического университета, 2018 The principle scheme of the stand is оffered for test the hydraulic machines with economy of the energy. Happens to its mathematical model and information about its preliminary analysis.
A.T. RYBAK, A.V. SERDYUKOV
doaj
An analysis of cross-coupling of a multicomponent jet engine test stand using finite element modeling techniques [PDF]
A two axis thrust measuring system was analyzed by using a finite a element computer program to determine the sensitivities of the thrust vectoring nozzle system to misalignment of the load cells and applied loads, and the stiffness of the structural ...
Schweikhard, W. G., Singnoi, W. N.
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Measured and predicted shock shapes for AFE configuration at Mach 6 in air and in CF4 [PDF]
Shock shapes and stand-off distances were obtained for the Aeroassist Flight Experiment configuration from Mach 6 tests in air and in CF4. Results were plotted for an angle-of attack range from -10 to 10 degrees and comparisons were made at selected ...
Franks, Alan M., Wells, William L.
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An open-source test stand for backlash measurement in low-cost UART servo motors. [PDF]
HardwareXKotov B.
europepmc +1 more source
Vibration Analysis of Aviation Electric Propulsion Test Stand with Active Main Rotor. [PDF]
Sensors (Basel)Kliza R +3 more
europepmc +1 more source