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Christopher M. Heath
Christopher M. Heath
NASA Glenn Research Center
Verified email at nasa.gov
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Cited by
Year
OpenMDAO: framework for flexible multidisciplinary design, analysis and optimization methods
C Heath, J Gray
53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials …, 2012
592012
Optical characterization of a multipoint lean direct injector for gas turbine combustors: Velocity and fuel drop size measurements
CM Heath, YR Hicks, RC Anderson, RJ Locke
Turbo Expo: Power for Land, Sea, and Air 43970, 791-802, 2010
412010
Conceptual feasibility study of the hyperloop vehicle for next-generation transport
K Decker, J Chin, A Peng, C Summers, G Nguyen, A Oberlander, G Sakib, ...
AIAA SciTech 2017, 2017
402017
Investigations of a combustor using a 9-point swirl-venturi fuel injector: recent experimental results
YR Hicks, CM Heath, RC Anderson, KM Tacina
20th International Symposium on Air Breathing Engines (ISABE 2011), 2012
322012
Characterization of swirl-venturi lean direct injection designs for aviation gas turbine combustion
CM Heath
Journal of Propulsion and Power 30 (5), 1334-1356, 2014
222014
Aerodynamic shape optimization of a two-stream supersonic plug nozzle
C Heath, EJ Nielsen, MA Park, JS Gray
53rd AIAA Aerospace Sciences Meeting, 1047, 2015
202015
Inlet trade study for a low-boom aircraft demonstrator
CM Heath, JW Slater, SK Rallabhandi
Journal of Aircraft 54 (4), 1283-1293, 2017
192017
Laboratory and modeling studies on the effects of water and soot emissions and ambient conditions on the properties of contrail ice particles in the jet regime
HW Wong, AJ Beyersdorf, CM Heath, LD Ziemba, EL Winstead, ...
Atmospheric Chemistry and Physics 13 (19), 10049-10060, 2013
152013
Viscous aerodynamic shape optimization with installed propulsion effects
C Heath, J Seidel, SK Rallabhandi
35th AIAA Applied Aerodynamics Conference, 3046, 2017
102017
Design and analysis of an isokinetic sampling probe for submicron particle measurements at high altitude
CM Heath
82012
System-level impact of propulsive uncertainties for low-boom aircraft concepts
BD Phillips, C Heath
AIAA AVIATION 2020 FORUM, 2730, 2020
72020
Wedge shock and nozzle exhaust plume interaction in a supersonic jet flow
R Castner, K Zaman, A Fagan, C Heath
Journal of Aircraft 54 (1), 125-134, 2017
72017
Conceptual sizing and feasibility study for a magnetic plane concept
K Decker, J Chin, A Peng, C Summers, G Nguyen, A Oberlander, G Sakib, ...
55th AIAA aerospace sciences meeting, 0221, 2017
62017
Parametric modeling investigation for radially staged low-emission combustion
CM Heath
Journal of Propulsion and Power 32 (2), 500-515, 2016
62016
Parametric modeling investigation of a radially-staged low-emission aviation combustor
C Heath
54th AIAA aerospace sciences meeting, 1394, 2016
52016
Evolution of combustion-generated particles at tropospheric conditions
KM Tacina, CM Heath
Turbo Expo: Power for Land, Sea, and Air 43970, 1289-1299, 2010
42010
Numerical Simulations of a Quiet SuperSonic Technology (QueSST) Aircraft Preliminary Design
DJ Friedlander, C Heath, RS Castner
2018 Fluid Dynamics Conference, 3861, 2018
32018
Tilter motor cooling apparatus for vertical takeoff and landing aircraft and operating method of the same
B Tulsyan, CM Heath, K Manning, G Droandi
US Patent 11,679,872, 2023
22023
Systems and methods for lifter motor cooling in eVTOL aircraft
KK Bodla, B Tulsyan, CM Heath, K Manning, AD Tepe
US Patent 11,613,350, 2023
22023
System and Methods for Lifter Motor Cooling in EVTOL Aircraft
KK Bodla, B Tulsyan, CM Heath, K Manning, AD Tepe
US Patent App. 18/163,372, 2024
2024
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