High Stability Engine Control (HISTEC) : flight demonstration results /

Imaging of combustion species in a radially-staged gas turbine combustor /
by: Locke, Randy J.
Published: (1996)

Numerical assessment of four-port through-flow wave rotor cycles with passage height variation /
by: Paxson, Daniel E., et al.
Published: (1997)

Performance of a high-work, low-aspect-ratio turbine tested with a realistic inlet radial temperature profile /
by: Stabe, Roy G.
Published: (1984)

Experimental determination of gap flow-conditioned forces at turbine stages and their effect on the running stability of simple rotors /
by: Wohlrab, Raimund
Published: (1983)

Wave-rotor-enhanced gas turbine engine demonstrator /
by: Welch, Gerard E.
Published: (1999)

Aerothermal modeling : phase I final report : executive summary /
by: Kenworthy, M. K., et al.
Published: (1983)

Application of a Constant Gain Extended Kalman Filter for in-flight estimation of aircraft engine performance parameters /
by: Kobayashi, Takahisa
Published: (2005)

Recent progress in research pertaining to estimates of gas-side heat transfer in an aircraft gas turbine /
by: Graham, Robert W.
Published: (1990)

Reducing aviation fuel costs with non-destructive testing /
by: Schemmel, Peter J.
Published: (2019)

High pressure turbine test hardware detailed design report /
by: Halila, E. E., et al.
Published: (1982)

A guide to axial-flow turbine off-design computer program AXOD2 /
by: Chen, Shu-cheng S.
Published: (2014)

Challenges to laser-based imaging techniques in gas turbine combustor systems for aerospace applications /
by: Locke, Randy J.
Published: (1998)

Capability extension to the turbine off-design computer program AXOD with applications to the highly loaded fan-drive turbines /
by: Chen, Shu-cheng S.
Published: (2011)

Experiments in dilution jet mixing /
by: Holdeman, J. D.
Published: (1983)

Effects of gas turbine component performance on engine and rotary wing vehicle size and performance /
by: Herrick, Gregory P.
Published: (2010)

Shock position control for mode transition in a turbine based combined cycle engine inlet model /
by: Csank, Jeffrey T., et al.
Published: (2013)

Advanced shock position control for mode transition in a turbine based combined cycle engine inlet model /
by: Csank, Jeffrey T., et al.
Published: (2013)

Dynamic testing of the NASA Hypersonic Project combined cycle engine testbed for mode transition experiments /
Published: (2011)

Detection of the impact of ice crystal accretion in an aircraft engine compression system during dynamic operation /
by: May, Ryan D., et al.
Published: (2014)

Advanced Turbine Technology (ATTAP) Applications Project : 1989 annual report /
Published: (1990)

Analysis of coupled seals, secondary and powerstream flow fields in aircraft and aerospace turbomachines /
by: Athavale, M. M.
Published: (2005)

Determination of the static performance of a Cuyuna 430 cc. model UL-430RR engine /
by: Roskam, Jan, 1930-
Published: (1983)

Non-intrusive, laser-based imaging of Jet-A fuel injection and combustion species in high pressure, subsonic flows /
Published: (2001)

Energy efficient engine high pressure turbine component rig performance test report /
by: Leach, K. P.
Published: (1983)

The effects of Reynolds number, rotor incidence angle and surface roughness on the heat transfer distribution in a large-scale turbine rotor passage /
by: Blair, M. F.
Published: (1991)

The effects of Reynolds number, motor incidence angle and surface roughness on the heat transfer distribution in a large-scale turbine rotor passage /
by: Blair, M. F.
Published: (1991)

Understanding and mitigating tip leakage and endwall losses in high pressure ratio cores /
by: Christophel, Jesse
Published: (2015)

Computational analyses of the LIMX TBCC inlet high-speed flowpath /
by: Dippold, Vance
Published: (2012)

Advanced Turbine Technology (ATTAP) Applications Project : 1988 annual report /
Published: (1989)

DBD plasma actuators for flow control in air vehicles and jet engines : simulation of flight conditions in test chambers by density matching /
by: Ashpis, D. E. (David E.)
Published: (2011)

DBD plasma actuators for flow control in air vehicles and jet engines : simulation of flight conditions in test chambers by density matching /
by: Ashpis, D. E. (David E.), et al.
Published: (2011)

Multipoint design and optimization of a turboshaft engine for a tiltwing turboelectric vertical takeoff landing air taxi /
by: Chapman, Jeffryes W.
Published: (2019)

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

A simplified model for detonation based pressure-gain combustors /
by: Paxson, Daniel E.
Published: (2010)

Turbine engine clearance control systems : current practices and future directions /
by: Lattime, Scott B.
Published: (2002)

Turbine engine clearance control systems : current practices and future directions /
by: Lattime, Scott B., et al.
Published: (2002)