Books on the topic 'Hydrogen injection'

P, Waltman Donna, Hillman Daniel C, and Environmental Monitoring Systems Laboratory (Las Vegas, Nev.), eds. The determination of pH by flow injection analysis and by fiber optrode analysis. Las Vegas, Nev: Environmental Monitoring Systems Laboratory, Office of Research and Development, U.S. Environmental Protection Agency, 1988.

Gerke, Udo. Numerical analysis of mixture formation and combustion in a hydrogen direct-injection internal combustion engine. Göttingen: Cuvillier, 2007.

W, Nyland Ted, and United States. National Aeronautics and Space Administration., eds. Hydrogen no-vent fill testing in a 5 cubic foot (142) liter tank using spray nozzle and spray bar liquid injection. [Washington, DC]: National Aeronautics and Space Administration, 1992.

W, Nyland Ted, and United States. National Aeronautics and Space Administration., eds. Hydrogen no-vent fill testing in a 5 cubic foot (142) liter tank using spray nozzle and spray bar liquid injection. [Washington, DC]: National Aeronautics and Space Administration, 1992.

W, Nyland Ted, and United States. National Aeronautics and Space Administration., eds. Hydrogen no-vent fill testing in a 5 cubic foot (142) liter tank using spray nozzle and spray bar liquid injection. [Washington, DC]: National Aeronautics and Space Administration, 1992.

Dresar, Neil T. Van. Prediction of pressurant mass requirements for axisymmetric liquid hydrogen tanks. [Washington, DC]: National Aeronautics and Space Administration, 1995.

J, Breisacher Kevin, and United States. National Aeronautics and Space Administration., eds. A comparison of analytical results for 20 K LOX/hydrogen instabilities. [Washington, D.C.]: NASA, 1990.

J, Breisacher Kevin, and United States. National Aeronautics and Space Administration., eds. A comparison of analytical results for 20 K LOX/hydrogen instabilities. [Washington, D.C.]: NASA, 1990.

Austria) International Seminar "AVL Simulation Tools--Practical Applications" (2011 Graz. AVL simulation tools: Practical applications. Lublin: Politechnika Lubelska, 2012.

Moran, Matthew E. Liquid Transfer Cryogenic Test Facility: Initial hydrogen and nitrogen no-vent fill data. [Washington, D.C.]: NASA, 1990.

Domel, N. D. A two-dimensional numerical simulation of shock-enhanced mixing in a rectangular scramjet flowfield with parallel hydrogen injection. Washington, D. C: American Institute of Aeronautics and Astronautics, 1991.

United States. National Aeronautics and Space Administration., ed. Zero-G Thermodynamic Venting System (TVS) performance prediction program. Downey, Calif: Rockwell Aerospace, 1994.

Center, Lewis Research, ed. LOX/hydrogen coaxial injector atomization test program. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1990.

Cooper, C. David. A pilot-scale evaluation of a new technology to control NO(x) emissions from boilers at KSC: Hydrogen peroxide injection into boiler flue gases followed by wet scrubbing of acid gases : annual progress report. [Orlando, Fla.]: Civil & Environmental Engineering Dept., University of Central Florida, 1997.

United States. National Aeronautics and Space Administration., ed. A pilot-scale evaluation of a new technology to control NO(x) emissions from boilers at KSC: Hydrogen peroxide injection into boiler flue gases followed by wet scrubbing of acid gases : annual progress report. [Orlando, Fla.]: Civil & Environmental Engineering Dept., University of Central Florida, 1997.

United States. National Aeronautics and Space Administration., ed. A pilot-scale evaluation of a new technology to control NO(x) emissions from boilers at KSC: Hydrogen peroxide injection into boiler flue gases followed by wet scrubbing of acid gases : annual progress report. [Orlando, Fla.]: Civil & Environmental Engineering Dept., University of Central Florida, 1997.

Nair, Lakshmi S. Injectable hydrogels for regenerative engineering. Hackensack, NJ: Imperial College Press, 2016.

D, Smith Timothy, and NASA Glenn Research Center, eds. Experimental evaluation of a subscale gaseous hydrogen/gaseous oxygen coaxial rocket injector. Cleveland, Ohio: National Aeronautics and Space Administration, Glenn Research Center, 2002.

The determination of pH by flow injection analysis and by fiber optrode analysis: Project summary. Las Vegas, NV: U.S. Environmental Protection Agency, Environmental Monitoring Systems Laboratory, 1988.

Zero-G Thermodynamic Venting System (TVS) performance prediction program. Downey, Calif: Rockwell Aerospace, 1994.

Zero-G Thermodynamic Venting System (TVS) performance prediction program. Downey, Calif: Rockwell Aerospace, 1994.

Gaseous hydrogen/oxygen injector performance characterization. [Washington, DC]: National Aeronautics and Space Administration, 1994.

A pilot-scale evaluation of a new technology to control NO(x) emissions from boilers at KSC: Hydrogen peroxide injection into boiler flue gases followed by wet scrubbing of acid gases : annual progress report. [Orlando, Fla.]: Civil & Environmental Engineering Dept., University of Central Florida, 1997.

EXPERIMENTAL EVALUATION OF SUBSCALE GASEOUS HYDROGEN/GASEOUS OXYGEN COAXIAL ROCKET INJECTOR... NASA/TM--2002-211982... NATIONAL AERONAUTICS. [S.l: s.n., 2003.

Thruster injector faceplate testing in support of the aerojet Rocket-based combined cycle (RBCC) concept. [Marshall Space Flight Center, Ala.]: National Aeronautics and Space Administration, Marshall Space Flight Center, 1998.