Users manual for free vibration analysis of stiffened cylinders with an attached weight
Computer program handbook for free vibration analysis of stiffened cylinders with attached weight
Davis, S.↗
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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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Microprobe Attachment for Quantitative Studies of Cathode Luminescence
Monochromator photomultiplier attachment to electron microprobe for measuring luminescence of enstatite
Greer, R. T.↗
Study of attachment methods for advanced spacecraft thermal-control materials Final report
Attachment methods for thermal control composite system comprised of optical solar reflectors and multilayer insulation to minimize heating from incident solar energy
Kordsmeir, N. H., Jr.↗
Summary of the development status of attached inflatable decelerators.
Structural and aerodynamic developments in attached inflatable decelerators for deployment of payload at supersonic speeds
Bohon, H. L.↗
Formal problems in the theory of dissociative attachment and recombination.
Dissociative attachment and recombination, discussing resonance state joining and asymptotic physical state and projection operator techniques
Chen, J. C. Y.↗
Attached flow gust penetration loads
Attached flow gust loads of slender bodies moving supersonic speeds
Scholnick, I. M.↗
Flight-measured aerodynamic drag of two large external tanks attached to the X-15-2 airplane at Mach numbers of 1.6 to 2.3
Aerodynamic drag of external fuel tanks attached to X-15-2 airplane at Mach numbers of 1.6 to 2.3
Fisher, D. F.↗
Injection of an attached inviscid jet at an oblique angle to a moving stream
Injection of attached inviscid jet at oblique angle to moving stream
Braun, W.↗
A method for computing the response of a general axisymmetric shell with an attached asymmetric structure.
Dynamic analysis of axisymmetric ring stiffened shells with attached asymmetric elastic structures, noting vibration modes
Durling, B. J.↗
Variables affecting the dynamic response of thermocouples attached to thin-skinned models.
Thermocouples dynamic response attached to thin skinned model under constant heating rate, considering error reduction in temperature measurement
Larson, M. B.↗
Development status of attached inflatable decelerators.
Structural and aerodynamic developments in attached inflatable decelerators for deployment of payload at supersonic speeds
Bohon, H. L.↗
Electrical test wire attachment device
Test lead wire attachment quickly and securely engages screw head by expansion against the side walls of the screw head slot. Heat shrinkable tubing is used for the forward and shaft ends to insulate the device from accidental contact.
Ferry, R. T.↗
Vibration characteristics of a cylinder partially filled with liquid with an attached elastic drain pipe
Liquid and ullage gas effects of partially filled cylinder with attached elastic drain pipe
Kroll, R. J.↗
Static aerodynamic characteristics, pressure distributions, and ram-air inflation of attached inflatable decelerator models at Mach 3.0
Static aerodynamic characteristics, pressure distributions, and ram air inflation of attached inflatable drag chute models at supersonic speed
Deveikis, W. D.↗
Deployment and performance characteristics of 5-foot diameter /1.5 m/ attached inflatable decelerators from Mach number 2.2 to 4.4
Deployment and steady state performance of supersonic attached inflatable decelerator canopy models
Bohon, H. L.↗
Effect of strain-gage attachment by spotwelding and bonding on fatigue behavior of Ti-6Al-4V, Rene 41, and Inconel X
Effect of strain gage attachment by spotwelding and bonding on fatigue behavior of Ti-6Al-4V, Rene 41, and Inconel X
Imig, L. A.↗
Attached Inflatable Decelerator performance evaluation and mission-application study
Attached Inflatable Decelerator for planetary atmospheric entry, discussing mission applications and wind tunnel models performance
Bohon, H. L.↗
Wall attachment, flueric crossover ''AND'' gate
Gate performance is not adversely affected by normal dimensional variations encountered in fabrication and it operates throughout full loading range. Flow from one control must be sufficiently monostable to allow initial attachment and upon switching, return to outer wall. Venting must be adequate.
Hellbaum, R. F.↗