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Library


Links

http://www.spl.ch/publication/


http://www.arocket.net/library/

Here are 2 links to websites with extensive NASA documents

Library                       

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

-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

http://www.llnl.gov/tid/lof/

Plasma Reactor

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

Many of these documents are in PDF format

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

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


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