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Results for “Segments”

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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At least 1,585 records · Page 88

All sources NASA NTRS DOE OSTI

NASA NTRS1963

Computation of segmented approximations

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Lawson, C.↗

NASA NTRS1965

Juncture stress fields in multicellular shell structures. Volume VIII - Buckling analysis of segmental orthotropic cylinders under non-uniform stress distribution Final technical report

Orthotropic cylindrical shell buckling under axial compression - structural dynamics

STRUCTURAL DYNAMICS↗

NASA NTRS1965

Juncture stress fields in multicellular shell structures. Volume VII - Buckling analysis of segmental orthotropic cylinders under uniform stress distribution Final report

Theoretical solution for buckling problem of orthotropic cylindrical panels under axial compression

CURVED PANEL↗

NASA NTRS1967

Technique for verifying structural integrity of full-scale segments of launch vehicles at transonic speeds

Validity of testing full scale flight components in transonic wind tunnel by evaluating flow deviations from free flight in critical transonic phase of flight

FLIGHT STABILITY TEST↗

NASA NTRS1967

A new method for treating optimal trajectories with restricted segments

New method for treating optimal trajectories

EULER EQUATION↗

NASA NTRS1967

Engineering estimates for supersonic flutter of curved shell segments

Engineering estimates for supersonic flutter of curved shell panels

Anderson, W. J.↗

NASA NTRS1965

Investigation methods of fabricating and joining large sandwich segments for forming common domes phase 4 monthly report, 1-31 oct. 1965

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Source record↗

NASA NTRS1968

The development of a segmented, axially conducting, pyrolytic graphite reaction control engine Quarterly report, 15 Sep. - 14 Dec. 1966

Fabrication and cold flow testing of integral spray injector for flight configuration of axially conducting rocket engine

Source record↗

NASA NTRS1967

The development of a segmented, axially conducting, pyrolytic graphite reaction control engine Quarterly report, 15 Dec. 1966 - 14 Mar. 1967

Development of integral spray injector for pyrolytic graphite reaction control engine

Source record↗

NASA NTRS1969

Force-penetration characteristics of a sand horizontally penetrated by plates, cones, and spherical segments

Force penetration characteristics of sand horizontally penetrated by various geometrically shaped models

Cox, W. R.↗

NASA NTRS1968

Lead telluride bonding and segmentation study Semiannual phase report, 1 Feb. - 31 Jul. 1968

Chemical and physical properties of Co-Si-Ge system and PbTe-MnTe system, and life testing of thermocouples

Bates, H.↗

NASA NTRS1969

Lead telluride bonding and segmentation study Semiannual phase report no. 3, 1 Aug. 1968 - 31 Jan. 1969

Design and tests of thermoelectric systems with germanium silicon or lead telluride

Bates, H.↗

NASA NTRS1970

Swirl-can combustor segment

Combustor produces uniform circumferential and radial combustor exit temperature profiles and high combustion efficiency at high temperature loads. Absence of diluent air entry ports eliminates stress concentration points, low pressure fuel alleviates nozzle fouling, and abundant air at all burning stages reduces smoke.

Jones, R.↗

NASA NTRS1969