Fuel injector design optimization for an annular scramjet geometry /

Further shock tunnel studies of scramjet phenomena /
Published: (1986)

Further shock tunnel studies of scramjet phenomena /
Published: (1986)

Photographic study of liquid-oxygen boiling and gas injection in the injector of a chugging rocket engine /
by: Conrad, E. William, et al.
Published: (1964)

Experimental evaluation of a subscale gaseous hydrogen/gaseous oxygen coaxial rocket injector /
by: Smith, Timothy D.
Published: (2002)

Experimental evaluation of a subscale gaseous hydrogen/gaseous oxygen coaxial rocket injector /
Published: (2002)

Multidisciplinary analysis of a hypersonic engine /
by: Stewart, Mark E. M.
Published: (2002)

Multidisciplinary analysis of a hypersonic engine /
Published: (2002)

Thruster injector faceplate testing in support of the aerojet rocket-based combined cycle (RBCC) concept /
by: Fazah, M. M.
Published: (1998)

Computational analysis of the combustion process in an axisymmetric RBCC flowpath /
by: Steffen, Christopher J.
Published: (2001)

Computational analysis of the combustion process in an axisymmetric,RBCC flowpath /
by: Steffen, Christopher J., et al.
Published: (2001)

Three dimensional numerical simulation of rocket-based combined-cycle engine response during mode transition events /
by: Edwards, Jack R.
Published: (2003)

Development of advanced low emission injectors and high-bandwidth fuel flow modulation valves /
by: Mansour, Adel
Published: (2015)

Conjugate heat transfer analyses on the manifold for ramjet fuel injectors /
by: Wang, Xiao-Yen J.
Published: (2006)

Current status of superheat spray modeling with NCC /
by: Raju, M. S.
Published: (2012)

Dual-pump CARS development and application to supersonic combustion /
by: Magnotti, Gaetano, et al.
Published: (2012)

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

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

Testing of the NASA Hypersonics project's Combined Cycle Engine Large Scale Inlet Mode Transition Experiment (CCE LIMX) /
Published: (2012)

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

LOX/hydrogen coaxial injector atomization test program /
by: Zaller, M.
Published: (1990)

Highlights from a Mach 4 experimental demonstration of inlet mode transition for Turbine-Based Combined Cycle hypersonic propulsion /
by: Foster, Lancert E.
Published: (2012)

Low loss injector for space shuttle main engine : final report /
by: Von Pragenau, George L.
Published: (1984)

Langley mach 4 scramjet test facility /
Published: (1985)

Mach 10 experimental database of a three-dimensional scramjet inlet flow field /
by: Holland, Scott D.
Published: (1995)

Interaction of two-dimensional transverse jet with a supersonic mainstream /
by: Kraemer, G. O., et al.
Published: (1983)

Computational fluid dynamics (CFD) simulation of hypersonic turbine-based combined-cycle (TBCC) inlet mode transition /
by: Slater, John W.
Published: (2010)

Assessment of some atomization models used in spray calculations /
by: Raju, M. S.
Published: (2011)

Fundamental study of a single point lean direct injector part I : effect of air swirler angle and injector tip location on spray characteristics /
by: Tedder, Sarah A.
Published: (2015)

Space station hydrogen/oxygen thruster technology /
by: Briley, G. L.
Published: (1988)

Conceptual model of turbulent flameholding for scramjet combustors /
by: Huber, Paul W. (Paul William), 1920-
Published: (1980)

Development of a flush airdata sensing system on a sharp-nosed vehicle for flight at Mach 3 to 8 /
by: Davis, Mark C.
Published: (2000)

LOX/Hydrocarbon combustion instability investigation /
by: Jensen, R. J.
Published: (1989)

Simulations of spray reacting flows in a single element LDI injector with and without invoking an Eulerian scalar PDF method /
by: Shih, Tsan-Hsing, 1940-
Published: (2012)

Temperature and species measurements of combustion produced by a 9-point lean direct injector /
by: Tedder, Sarah A., et al.
Published: (2013)

Multifidelity analysis and optimization for supersonic design /
Published: (2010)

Nonsteady flame propagation
Published: (1964)