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NASA Scientific and Technical Aerospace Reports

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20040073730 Stanford Univ., Stanford, CA<br />

Interpreting Shock Tube Ignition Data<br />

Davidson, D. F.; Hanson, R. K.; Oct. 2003; 24 pp.; In English; Original contains color illustrations<br />

Contract(s)/Grant(s): DAAD19-01-1-0597<br />

Report No.(s): AD-A422646; 03F-61; ARO-41100.4-EG; No Copyright; Avail: CASI; A03, Hardcopy<br />

Chemical kinetic modelers make extensive use of shock tube ignition data in the development <strong>and</strong> validation of<br />

combustion reaction mechanisms. These data come from measurements using a range of diagnostics <strong>and</strong> a variety of shock<br />

tubes, fuels, <strong>and</strong> initial conditions. With the wide selection of data available, it is useful to realize that not all of the data are<br />

of all the same type or quality, nor are all the data suitable for simple, direct comparison with the predictions of reaction<br />

mechanisms. We present here a discussion of some guidelines for the comparison of shock tube ignition time data with<br />

reaction mechanism modeling. Areas discussed include: definitions of ignition time; ignition time correlations (with examples<br />

taken from recent n-heptane <strong>and</strong> iso-octane measurements); shock tube constant-volume behavior; shock tube diameter <strong>and</strong><br />

boundary layer effects; carrier gas <strong>and</strong> impurity effects; <strong>and</strong> future needs <strong>and</strong> challenges in shock tube research.<br />

DTIC<br />

Ignition; Shock Tubes<br />

20040073733 Massachusetts Inst. of Tech., Cambridge, MA<br />

Kinetics of Chemical Agents Destruction in Supercritical Water<br />

Tester, Jefferson W.; Sullivan, Patricia A.; Ploeger, Jason M.; Lachance, Russell P.; Dec. 31, 2003; 21 pp.; In English; Original<br />

contains color illustrations<br />

Contract(s)/Grant(s): DAAD19-99-1-0211<br />

Report No.(s): AD-A422649; ARO-39250.6-CH; No Copyright; Avail: CASI; A03, Hardcopy<br />

The work accomplishments during this project consist of five different studies conducted by three current PhD students<br />

in the laboratory. An experimental study of methylphosphonic acid (MPA) oxidation has been completed that includes<br />

macroscopic modeling of the overall global rate law for MPA oxidation in supercritical water (SCW) <strong>and</strong> for the major<br />

pathways in MPA oxidation. Additionally, an elementary reaction rate model for supercritical water oxidation (SCWO) of<br />

MPA has been developed consisting of rate parameters from the available literature <strong>and</strong> ab initio calculations. Urea hydrolysis<br />

kinetics have been experimentally measured at sub <strong>and</strong> supercritical water conditions. Additionally, recent studies in the<br />

laboratory include a co-oxidation stud of MPA <strong>and</strong> ethanol kinetics in SCW <strong>and</strong> a methane SCWO experimental study.<br />

DTIC<br />

Destruction; Oxidation; Reaction Kinetics; Water<br />

20040073746 Air Force Research Lab., Edwards AFB, CA<br />

Polynitrogen <strong>and</strong> High Nitrogen Chemistry: A New World of Challenges<br />

Vij, Ashwani; Mar. 25, 2004; 85 pp.; In English; Original contains color illustrations<br />

Contract(s)/Grant(s): Proj-DARP<br />

Report No.(s): AD-A422668; No Copyright; Avail: CASI; A05, Hardcopy<br />

Polynitrogen compounds contain only nitrogen atoms <strong>and</strong> are expected to have unusual properties. Most important among<br />

these are: High endothermicity Green propellant combustion product is only gaseous N2 High density High Isp values when<br />

compared to other monopropropellants or bipropellants High detonation velocity<br />

DTIC<br />

High Energy Propellants; Nitrogen; Synthesis (Chemistry)<br />

20040073756 Engineering Research <strong>and</strong> Consulting, Inc., Huntsville, AL<br />

Preparation <strong>and</strong> Characterization of the First Binary Titanium Azides, Ti(N3)4, P(C6H5)4Ti(N3)5 <strong>and</strong><br />

P(C6H5)42Ti(N3)6 <strong>and</strong> on Linear Ti-N-NN Coordination<br />

Christe, Karl O.; Haiges, Ralf; Schneider, Stefan; Schroer, Thorsten; Boatz, Jerry A.; Mar. 12, 2004; 21 pp.; In English;<br />

Original contains color illustrations<br />

Contract(s)/Grant(s): F04611-99-C-0025; Proj-DARP<br />

Report No.(s): AD-A422680; No Copyright; Avail: CASI; A03, Hardcopy<br />

Where as numerous partially azide-substituted titanium compounds had previously been reported, 1-7 no binary titanium<br />

azides were known. In a recent theoretical study the group 4 metal tetrazides M(N3)4 (M = Ti, Zr, Hf, Th) were predicted 8<br />

to be vibrationally stable exhibiting tetrahedral structures with unique linear M-N-NN bond angles (see Figure 1). All<br />

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