A program is described which seeks to develop an understanding of the effects of dissolved and trapped hydrogen on the mechanical properties of selected Al-Li-Cu-X alloys. A proposal is made to distinguish hydrogen (H2) induced EAC from aqueous dissolution controlled EAC, to correlate H2 induced EAC with mobile and trapped concentrations, and to identify significant trap sites and hydride phases (if any) through use of model alloys and phases. A literature review shows three experimental factors which have impeded progress in the area of H2 EAC for this class of alloys. These are as listed: (1) inter-subgranular fracture in Al-Li alloys when tested in the S-T orientation in air or vacuum make it difficult to readily detect H2 induced fractu...
Stem cells occupy variable environments where they must distinguish stochastic fluctuations from dev...
Fuel cell electrolyte properties - solubility of hydrogen and oxygen in KOH and LiOH, diffusivity of...
Complexities of liquid rocket engine heat transfer which involve the injector faceplate and regenera...
Information is given in viewgraph form on the heat generation during overcharge of nickel hydrogen c...
As a result of high cycle fatigue, hydrogen embrittlement, and extended engine use, it was observed ...
Asymptotic formulas for the characteristic root errors as well as transfer function gain and phase e...
This addendum is an update to 501 B for Heat Flow Experiment (HFE), Array A-2, D, E. Contained in th...
The investigation of machine-countersunk flush rivets for aircraft described in reference 1 revealed...
The use of lunar surface photography to achieve the photogrammetric transfer of available selenograp...
The guidelines for EVA and IVA tasks to be performed on the space shuttle are defined. In deriving t...
The topics addressed are: (1) Terminal Doppler Weather Radar (TDWR) 1991 program review; (2) TDWR de...
Test results for FM 5064 J (HITCO) Lots No. 1 (H) - 4 (H) for filler testing, resin testing, fabric ...
Following the start of SSME certification testing for the Pratt and Whitney Alternate Turbopump Deve...
Gravity gradient stabilization is planned for the space station. Torques arise from air-drag since t...
A code for calculating ultrasonic fields has been developed by revising the thermal-hydraulics-struc...
Stem cells occupy variable environments where they must distinguish stochastic fluctuations from dev...
Fuel cell electrolyte properties - solubility of hydrogen and oxygen in KOH and LiOH, diffusivity of...
Complexities of liquid rocket engine heat transfer which involve the injector faceplate and regenera...
Information is given in viewgraph form on the heat generation during overcharge of nickel hydrogen c...
As a result of high cycle fatigue, hydrogen embrittlement, and extended engine use, it was observed ...
Asymptotic formulas for the characteristic root errors as well as transfer function gain and phase e...
This addendum is an update to 501 B for Heat Flow Experiment (HFE), Array A-2, D, E. Contained in th...
The investigation of machine-countersunk flush rivets for aircraft described in reference 1 revealed...
The use of lunar surface photography to achieve the photogrammetric transfer of available selenograp...
The guidelines for EVA and IVA tasks to be performed on the space shuttle are defined. In deriving t...
The topics addressed are: (1) Terminal Doppler Weather Radar (TDWR) 1991 program review; (2) TDWR de...
Test results for FM 5064 J (HITCO) Lots No. 1 (H) - 4 (H) for filler testing, resin testing, fabric ...
Following the start of SSME certification testing for the Pratt and Whitney Alternate Turbopump Deve...
Gravity gradient stabilization is planned for the space station. Torques arise from air-drag since t...
A code for calculating ultrasonic fields has been developed by revising the thermal-hydraulics-struc...
Stem cells occupy variable environments where they must distinguish stochastic fluctuations from dev...
Fuel cell electrolyte properties - solubility of hydrogen and oxygen in KOH and LiOH, diffusivity of...
Complexities of liquid rocket engine heat transfer which involve the injector faceplate and regenera...