Cover Image

Approximation of engine casing temperature constraints for casing mounted electronics /

Bibliographic Details
Main Authors:	Kratz, Jonathan L. (Author), Culley, Dennis E. (Author), Chapman, Jeffryes W. (Author)
Format:	Government Document eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, April 2017.
Series:	NASA technical memorandum ; 2017-219477.
Subjects:	Combustion chambers. Heat transfer. In-flight simulation. Propulsion system performance. Temperature profiles. Weight analysis.
Online Access:	https://purl.fdlp.gov/GPO/gpo81330 http://purl.fdlp.gov/GPO/gpo81330

Similar Items

Beta testing of CFD code for the analysis of combustion systems /
by: Yee, Emma, et al.
Published: (2015)

Funding and strategic alignment guidance for infusing small business innovation research technology into NASA programs associated with the Human Exploration and Operations Mission Directorate /
by: Nguyen, Hung D., et al.
Published: (2015)

Metallized gelled propellants : oxygen/RP-1/aluminum rocket heat transfer and combustion measurements /
by: Palaszewski, Bryan Alan Richard, et al.
Published: (1996)

Numerical study of stratified charge combustion in wave rotors /
by: Nalim, M. Razi
Published: (1997)

Optical characterization of a multipoint lean direct injector for gas turbine combustors : velocity and fuel drop size measurements /
Published: (2010)

Ten year operating test results and post-test analysis of a 1/10 segment stirling sodium heat pipe : phase III final report /
by: Rosenfeld, John H., et al.
Published: (2012)

Flame radiation and liner heat transfer in a tubular-can combustor /
by: Claus, Russell W.
Published: (1984)

High temperature furnace modeling and performance verifications : semi-annual progress report, NAG8-5 /
by: Smith, James E.
Published: (1991)

Effects of spent cooling and swirler angle on a 9-point swirl-venturi injector /
by: He, Zhuohui J.
Published: (2014)

High-temperature optical window design.
by: Roeloffs, Norman
Published: (1995)

NESC review of the 8-Foot High Temperature Tunnel (HTT) oxygen storage pressure vessel inspection requirements /
Published: (2009)

Burner liner thermal/structural load modeling /
by: Maffeo, R.
Published: (1984)

Prevention of over-pressurization during combustion in a sealed chamber /
by: Gokoglu, Suleyman A.
Published: (2012)

Full-scale turbofan engine noise-source separation using a four-signal method /
by: Hultgren, Lennart S. (Lennart Sven), et al.
Published: (2016)

High-temperature, oxidation-rersistant thruster research /
by: Wooten, J. R.
Published: (1990)

Optically based flame detection in the NASA Langley 8-ft high-temperature wind tunnel /
by: Borg, Steven E.
Published: (2005)

Investigations of a combustor using a 9-point swirl-venturi fuel injector : recent experimental results /
Published: (2012)

Summary of pressure gain combustion research at NASA /
by: Perkins, Hugh Douglas, et al.
Published: (2018)

A radiation solver for the national combustion code /
by: Sockol, Peter M.
Published: (2015)

Ames Research Center shear tests of SLA-561V heat shield material for Mars-Pathfinder /
by: Tran, Huy
Published: (1996)

BOREAS AFM-06 mean temperature profile data /
by: Wilczak, James M.
Published: (2000)

BOREAS TGB-1/TGB-3 water table and peat temperature data over the NSA /
by: Bubier, Jill L., et al.
Published: (2000)

Design and verification by nonlinear simulation of a Mach/CAS control law for the NASA TSRV B-737 aircraft : final report /
by: Bruce, Kevin R.
Published: (1986)

A design methodology for rapid implementation of active control systems across lean direct injection combustor platforms /
by: Baumann, William T.
Published: (2003)

Flight simulator evaluation of enhanced propulsion control modes for emergency operation /
by: Litt, Jonathan S.
Published: (2012)

Comparison of Mars aircraft propulsion systems /
by: Colozza, Anthony J.
Published: (2003)

The structure of dilute combusting sprays /
by: Shuen, J.-S
Published: (1985)

The effect of air preheat at atmospheric pressure on the formation of NO[subscript x] in the quick-mix section of an axially staged combustor /
by: Vardakas, M. A.
Published: (1999)

Development of a gas-fed pulse detonation research engine /
by: Litchford, R. J.
Published: (2001)

Foundational performance analyses of pressure gain combustion thermodynamic benefits for gas turbines /
by: Paxson, Daniel E.
Published: (2012)

Temperature data assimilation with salinity corrections : validation for the NSIPP ocean data assimilation system in the tropical Pacific Ocean, 1993-1998 /
by: Troccoli, Alberto
Published: (2003)

The role of molecular weight and temperature on the elastic and viscoelastic properties of a glassy thermoplastic polyimide /
by: Nicholson, Lee M.
Published: (2001)

Orbit transfer vehicle engine technology program combustor wall condition monitoring, subtask II, task E.5 /
by: Szemenyei, B. L.
Published: (1988)

Near-net shape powder metallurgy rhenium thruster /
Published: (2001)

Near-net shape powder metallurgy rhenium thruster /
by: Leonhardt, Todd A.
Published: (2001)

Combustion in advanced gas turbine systems proceedings.
Published: (1968)

Integrated high payoff rocket propulsion technology (IHPRPT) SiC recession model /
by: Opila, E. (Elizabeth)
Published: (2009)

NASA one-dimensional combustor simulation : user manual for S1D_ML /
by: Stueber, Thomas J., et al.
Published: (2014)

Combustion dynamics characteristics and fuel pressure modulation responses of a three-cup third-generation swirl-venturi lean direct injection combustion concept /
by: He, Zhuohui J.
Published: (2020)

Optical flameout detector : patent application /
Published: (1993)