Development and comparison of advanced reduced-basis methods for the transient structural analysis of unconstrained structuresFormat: [microform] /
Author: McGowan, David M.
Publisher: [Springfield, Va. : National Technical Information Service, distributor, [Springfield, Va. : National Technical Information Service, distributor,
Date: 1993] This title can be found in 2 Iowa libraries.
A simplified method for thermal analysis of a cowl leading edge subject to intense local shock-wave-interference heating /Publisher: [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program,
Date: 1992. This title can be found in 1 Iowa libraries.
Development of advanced modal methods for calculating transient thermal and structural response /Author: Camarda, Charles J.
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center,
Date: 1991] This title can be found in 1 Iowa libraries.
Development of higher-order methods for transient thermal and structural analysisFormat: [electronic resource] /
Author: Camarda, Charles J.
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center,
Date: [1989] This title can be found in 1 Iowa libraries.
Application of formal optimization techniques in thermal/structural design of a heat-pipe-cooled panel for a hypersonic vehicle /Author: Camarda, Charles J.
Publisher: [Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Office,
Date: 1987. This title can be found in 1 Iowa libraries.
Development of higher-order methods for transient thermal and structural analysisFormat: [microform] /
Author: Camarda, Charles J.
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center,
Date: [1989] This title can be found in 1 Iowa libraries.
Static and dynamic structural-sensitivity derivative calculations in the finite-element-based engineering analysis language (EAL) system /Author: Camarda, Charles J.
Publisher: Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office,
Date: 1984. This title can be found in 1 Iowa libraries.
Tests of graphite/polymide sandwich panels in uniaxial edgewise compressionFormat: [microform] /
Author: Camarda, Charles J.
Publisher: Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch;
Date: 1980. This title can be found in 1 Iowa libraries.
Elevated-temperature application of the IITRI compression test fixture for graphite/polyimide filmentary compositesFormat: [microform] /
Author: Raju, B. Basava.
Publisher: Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ;
Date: 1979. This title can be found in 1 Iowa libraries.
Aerothermal tests of a heat-pine-cooled leading edge at Mach 7Format: [microform] /
Author: Camarda, Charles J.
Publisher: [Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ;
Date: 1978. This title can be found in 1 Iowa libraries.
Analysis and radiant heating tests of a heat-pipe-cooled leading edge /Author: Camarda, Charles J.
Publisher: Washington : National Aeronautics and Space Administration,
Date: 1977. This title can be found in 1 Iowa libraries.
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