First Investigation of Ducted Fuel Injection on a Retrofitted Heavy-Duty Multi-Cylinder Production Engine
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Mueller, Charles J. [Sandia National Laboratories ↗
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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Optical-Engine Study of the Effects of Polyoxymethylene Ether Fuel on Conventional Diesel Combustion & Ducted Fuel Injection
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Radhakrishna, Vishnu [Sandia National Laboratories↗
Automated Duct Sealing
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Iffa, Emishaw [ORNL]↗
The impact of pilot and post injections on ducted fuel injection performance
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Segatori, Cristiano [Politecnico di Torino]↗
Motion study of the suction ducting on the S-IC stage of the Saturn V vehicle
Method for determining axial and angular motion of each bellows in S-IC feed system of Saturn vehicle
ANGULAR MOTION↗
Swaged tube and duct connector feasibility
Design of fluid line connectors depending solely upon cold forming of metal to carry structural loads and to make helium leak-tight seal
SEALING↗
Effect of local pressure transients on the deformations and stresses in cylindrical ducts. Volume I - Theory and design charts
Axially symmetric dynamic response solutions for cylinders subjected to pressure transients arising in propulsion systems
PROPULSION SYSTEM↗
Effect of local pressure transients on the deformations and stresses in cylindrical ducts. Volume II - User's manual for general purpose program
Users manual for general purpose digital computer program for predicting dynamic response of cylinders subjected to ramp and sinusoidal pressure transients
DYNAMIC RESPONSE↗
Lower hybrid resonance noise and a new ionospheric duct.
Lower hybrid resonance in VLF range in satellites, noting noise emission due to trapping of electromagnetic wave propagation in transverse magnetic field
IONOSPHERIC PROPAGATION↗
Design, fabrication, and testing of pressurization and propellant feed ducting systems progress report no. 2, 1-31 aug. 1964
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Mischel, H. T.↗
Model tests of a wing-duct system for auxiliary air supply
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Bierman, D.↗
Digital computer program predicts effects of local pressure transients on deformation and stresses in cylindrical ducts
Digital computer program determines the dynamic response of circular cylinders subjected to pressure transient forms commonly encountered in propulsion systems. The method can be readily used to obtain solutions for all possible combinations of admissible boundary conditions.
Echenoz, Y.↗
Heat transfer to liquid-metal flow in a round tube or flat duct with heat sources in the fluid stream
Forced-convection heat-transfer characteristics of liquid metal flow in circular tube, and in parallel plate channel
HEAT TRANSFER↗
Zero Leakage Design for Ducts and Tube Connections for Deep Space Travel. Volume 4 - New Connector Designs and Testing Final Report, 5 Jul. 1963 - 30 Jun. 1967
Omega seal, diffusion bonded, pressure welded, and high temperature separable connector designs and environmental tests
Laniewski, J. P.↗
Zero leakage design for ducts and tube connections for deep space travel. Volume 1 - Fundamental investigations Final report, 5 Jul. 1963 - 30 Jun. 1967
Fundamental leakage and structural studies of fluid connectors and seals
Bain, J. A.↗
Zero leakage design for ducts and tube connections for deep space travel. Volume 5 - Tube connector design principles and evaluation Final report, 5 Jul. 1963 - 30 Jun. 1967
Principles of connector testing, design evaluation of commercial connectors, and assessment of design rules for threaded connectors
Bain, J. A.↗
Zero leakage design for ducts and tube connections for deep space travel. Volume 6 - X connector feasibility studies Final report, 5 Jul. 1963 - 30 Jun. 1967
Production design feasibility of half inch X-connector for 4500 psi service
Bain, J. A.↗
Secondary flow induced by a transverse resonant acoustic field in a circular duct.
Finite amplitude standing transverse resonant acoustic field effects upon flow behavior of viscous fluid in cylindrical enclosure to acoustically model combustion instability
Hribar, A. E.↗