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Here are 2 links to websites with extensive NASA documents |
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Library |
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The library section was created as a place for both our own research and to share with others the excellent sources of information we have found useful on the internet |

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-Nasa explanation of how a pitot tube measures airspeed http://www.lerc.nasa.gov/WWW/K-12/airplane/pitot.html -Nasa explanation of different types of rocket propulsion http://sec353.jpl.nasa.gov/apc/ LLNL library documents |
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Pulse Detonation Engines these documents were found at this link ADA380297 Design, Characterization, and Performance of a Valveless Pulse Detonation Engine ADA359179 Evaluation of a Liquid-Fueled Pulse Detonation Engine Combustor ADA380632 Influence Of Ignition Energy, Ignition Location, And Stoichiometry On The Deflagration-To- Detonation Distance In A Pulse Detonation Engine ADA381096 Propagation of a Two-Phase Detonation Across a Geometric Diffraction With Compositional Discontinuity |
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Many of these documents are in PDF format |
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Pulse Jets these documents were found at this link ADA377333 Investigation of the Propulsive Characteristics of a Helicopter Type Pulse Jet Engine over a Range of Mach Numbers and Angle of Yaw |
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Ram Jets these documents were found at this link ADA373397 Solid Fuel Ramjet Regulation by Means of an Air Division Valve ADA378536 Development of Shrouded Turbojet to Form a Turboramjet for Future Missile Applications ADA318443 Experimental Demonstration of a 120-mm Ram Accelerator. ADA353103 Thermal Performance of a Scramjet Combustor Operating at Mach 5.6 FlightConditions ADA356286 Hypersonic Missile Propulsion System ADA373370 Aerodynamic Performance Analysis of the Hypersonic Airbreathing Vehicle JAPHAR, ADA384476 Advanced Mixing of Fuel/Oxidant System in High Speed Gaseous Flows Stage1 ADA322023 Turbulent Reacting Flows at High Speed. ADA356336 Fundamental Investigations of an Integrated Fuel Injector/Flameholder Concept for Supersonic Combustion ADA358872 Spontaneous Ignition of Hydrocarbon Fuels at Temperatures in the Range 750 - 1500 K ADA361609 Heat Transfer to the Inclined Trailing Wall of an Open Cavity ADA364233 Finite Element Computation of the Dynamics of Large Ram Air Parachutes ADA368692 High Resolution Measurements of Supersonic Mixing and Combustion in Coflowing Turbulent Jets ADA370851 Performance of a Ducted Micro-Turbojet Engine ADA372847 Advanced Airbreathing Hydrocarbon-Fueled Aero-Engine Concepts ADA373274 Direct Fuel Cooled Composite Structure ADA378098 Flow Visualization of Four-Inlet Ducted Rocket Engine Configurations |
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Technical Report Servers http://www.ssl.umd.edu/space/reports.html Large List of Technical Reports Servers http://techreports.larc.nasa.gov/cgi-bin/NTRS NTRS - Nasa Technical Reports Server |