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Alternate Subjects (1-6 of 6)
Roller Bearings
1
E-Books/E-Docs
 

Comparison of predicted and measured temperatures of UH-60A helicopter transmission


Coe, Harold H.
[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989. 1989

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 Axe Federal Documents Online  NAS 1.60:2911    ---  Available
2
E-Books/E-Docs
 

Effect of cage design on characteristics of high-speed-jet-lubricated 35-millimeter-bore ball bearin


Schuller, Fredrick T., author.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, October 1980. 1980-

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 Axe Federal Documents Online  NAS 1.60:1732    ---  Available
3
E-Books/E-Docs
 

Modification of the SHABERTH bearing code to incorporate RP-1 and a discussion of the traction model


Woods, Claudia M.
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1990. 1990

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 Axe Federal Documents Online  NAS 1.60:3017    ---  Available
4
E-Books/E-Docs
 

Non-linear dynamic analysis of geared systems.


Singh, Rajendra.
[Columbus, Ohio] : The Ohio State University, Dept. of Mechanical Engineering ; Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, [1990] 1990

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 Axe Federal Documents Online  NAS 1.26:180495    ---  Available
5
E-Books/E-Docs
 

Review and critical analysis--rolling-element bearings for system life and reliability


Irwin, Arthur S.
[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, [1985] 1985

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 Axe Federal Documents Online  NAS 1.26:174710    ---  Available
6
E-Books/E-Docs
 

Rotorcraft transmission noise path model, including distributed fluid film bearing impedance modelin



Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2010] 2010

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 Axe Federal Documents Online  NAS 1.26:2010-216812    ---  Available
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