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Alternate Subjects (1-4 of 4)
Blade Tips
1
ElectronicResource GovDoc
 

Blade tip rubbing stress prediction final report


Davis, Gary A.
Canoga Park, Calif. : Rockwell International, Rocketdyne Division, [1991] 1991

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 Axe Federal Documents Online  NAS 1.26:184100    ---  Available
2
ElectronicResource GovDoc
 

Effects of tip clearance and casing recess on heat transfer and stage efficiency in axial turbines


Ameri, Ali A.
[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, [1998] 1998

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 Axe Federal Documents Online  NAS 1.26:208514    ---  Available
3
ElectronicResource GovDoc
 

Heat transfer and flow on the first stage blade tip of a power generation gas turbine.


Ameri, Ali A.
[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; [Hanover, Md. : NASA Center for Aerospace Information, distributor, 1999] 1999

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 Axe Federal Documents Online  NAS 1.26:209151/PT.2    ---  Available
4
ElectronicResource GovDoc
 

Large-scale Advanced Propfan (LAP) performance, acoustic and weight estimation, January, 1984


Parzych, David J.
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1985] 1985

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Location Call No. OPAC Message Status
 Axe Federal Documents Online  NAS 1.26:174782    ---  Available
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