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United Technologies Corporation Hamilton Standard Division
1
E-Books/E-Docs
 

Analysis and test evaluation of the dynamic stability of three advanced turboprop models at zero for


Smith, Arthur F.
Windsor Locks, Conn. : Hamilton Standard Division, United Technologies Corporation ; Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, [1985] 1985

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Location Call No. OPAC Message Status
 Axe Federal Documents Online  NAS 1.26:175025    ---  Available
2
E-Books/E-Docs
 

Large-scale advanced prop-fan (LAP) blade design


Sullivan, William E.
[Windsor Locks, Conn.?] : Hamilton Standard Division, United Technologies ; [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, [1984?] 1984

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Location Call No. OPAC Message Status
 Axe Federal Documents Online  NAS 1.26:174790    ---  Available
3
E-Books/E-Docs
 

Large-scale advanced prop-fan (LAP) ptich change actuator and control design report


Schwartz, Robert A.
[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, [1986] 1986

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 Axe Federal Documents Online  NAS 1.26:174788    ---  Available
4
E-Books/E-Docs
 

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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