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Displaying 1-11 of 11 results
NASA GRC's high pressure burner rig facility and materials test capabilities [microform] / R. Craig Robinson.
- Text
- [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
- 1999
Hot corrosion test facility at the NASA Lewis Special Projects Laboratory [microform] / Raymond C. Robinson and Michael D. Cuy.
- Text
- [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
- 1994
Corrosion of mullite by molten salts [microform] / Nathan S. Jacobson and Kang N. Lee ; Tetsuo Yoshio.
- Text
- [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
- 1996
Ensemble diffraction measurements of spray combustion in a novel vitialed coflow turbulent jet flame burner [microform] / R. Cobra ... [et al.] ; prepared for the spring meeting of the Western States Section of the Combustion Institute sponsored by the Combustion Institute, Golden, Colorado, March 13-14, 2000 ; prepared under grant NAG3-2103.
- Text
- [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2000]
- 2000
Experimental verification of corrosive vapor deposition rate theory in high veloicty burner rigs [microform] / Suleyman A. Gokoglu and Gilbert J. Santoro.
- Text
- [Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1986]
- 1986
Determination of convective diffusion heat/mass transfer rates to burner rig test targets comparable in size to cross-stream jet diameter [microform] / Suleyman A. Gokoglu and Gilbert J. Santoro.
- Text
- [Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1986]
- 1986
Experiments for the determination of convective diffusion heat/mass transfer to burner rig test targets comparable in size to jet stream diameter [microform] / Gilbert J. Santoro and Suleyman A. Gokoglu.
- Text
- [Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1986]
- 1986
Digital temperature and velocity control of Mach 0.3 atmospheric pressure durability testing burner rigs in long time, unattended cyclic testing [microform] / Daniel L. Deadmore.
- Text
- [Washington, D.C.] : National Aeronautics and Space Administration, [1985]
- 1985
Ribbon-burner simulation of the T-700 turbine shroud section for ceramic-lined seals research [microform] / J.K. Little ... [et al.].
- Text
- [Washington, D.C.] : National Aeronautics and Space Administration, [1985]
- 1985
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS104768Burner liner thermal/structural load modeling [microform] / by R. Maffeo.
- Text
- Cincinnati, OH : General Electric Co., Aircraft Engine Business Group, [1984]
- 1984
Simultaneous laser raman-rayleigh-LIF measurements and numerical modeling results of a lifted turbulent H₂/N₂ jet flame in a vitiated coflow / R. Cabra ... [and others].
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2002]
- 2002
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo27166
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