Livres sur le sujet « Hydrogen injection »

P, Waltman Donna, Hillman Daniel C et Environmental Monitoring Systems Laboratory (Las Vegas, Nev.), dir. 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, et United States. National Aeronautics and Space Administration., dir. 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, et United States. National Aeronautics and Space Administration., dir. 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, et United States. National Aeronautics and Space Administration., dir. 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, et United States. National Aeronautics and Space Administration., dir. A comparison of analytical results for 20 K LOX/hydrogen instabilities. [Washington, D.C.] : NASA, 1990.

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

Center, Lewis Research, dir. 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., dir. 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., dir. 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, et NASA Glenn Research Center, dir. 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.