45th AIAA Aerospace Sciences Meeting and Exhibit
45th AIAA Aerospace Sciences Meeting and Exhibit
45th AIAA Aerospace Sciences Meeting and Exhibit
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Monday Morning / 08 January 2007<br />
Session 29-WE-1 Aeroelastics <strong>and</strong> CFD McKinley<br />
Chaired by: J. JONKMAN <strong>and</strong> P. MORIARTY, National Renewable Energy Laboratory, Golden, CO<br />
0830<br />
<strong>AIAA</strong>-2007-0210<br />
Rigid Body Modeling of<br />
Wind Turbines for<br />
Aeroelastic Stability<br />
Investigations<br />
J. Holierhoek, Delft<br />
University of<br />
Technology, Delft, The<br />
Netherl<strong>and</strong>s<br />
0900<br />
<strong>AIAA</strong>-2007-0211<br />
Investigation into the<br />
Possibility of Flap- Lag-<br />
Stall Flutter<br />
J. Holierhoek, Delft<br />
University of<br />
Technology, Delft, The<br />
Netherl<strong>and</strong>s<br />
Monday Afternoon / 08 January 2007<br />
Session 31-AA-2 Airframe Noise: Flaps, Slats, <strong>and</strong> L<strong>and</strong>ing Gear N-10<br />
Monday Afternoon / 08 January 2007<br />
0930<br />
<strong>AIAA</strong>-2007-0212<br />
Development <strong>and</strong><br />
Verification of a Fully<br />
Coupled Simulator for<br />
Offshore Wind Turbines<br />
J. Jonkman, National<br />
Renewable Energy<br />
Laboratory, Golden, CO<br />
1000<br />
<strong>AIAA</strong>-2007-0213<br />
3D Rotational<br />
Corrections in ONERA<br />
Aeroelastic Predictions<br />
of NREL Wind Turbine<br />
M. Rapin, ONERA,<br />
Chatillon, France<br />
1030<br />
<strong>AIAA</strong>-2007-0216<br />
Numerical Simulation of<br />
Wind Turbine Scale<br />
Effects by Using CFD<br />
Y. Park, Korea<br />
<strong>Aerospace</strong> Research<br />
Institute, Daejon, South<br />
Korea<br />
Chaired by: R. STOKER, The Boeing Company, Seattle, WA, <strong>and</strong> J. DELFS, DLR, German <strong>Aerospace</strong> Research Center, Brunswick, Germany<br />
1330<br />
<strong>AIAA</strong>-2007-0224<br />
Flap- Edge Flowfield<br />
<strong>and</strong> Noise in Civil<br />
Transport Aircraft Model<br />
M. Kuroda, Tohoku<br />
University, Sendai,<br />
Japan<br />
1400<br />
<strong>AIAA</strong>-2007-0225<br />
Measurements of Flow<br />
Around a Split Flap<br />
Configuration<br />
,<br />
1430<br />
<strong>AIAA</strong>-2007-0226<br />
Simulation of the<br />
Broadb<strong>and</strong> Noise from a<br />
Slat Using Zonal<br />
LES/RANS Hybrid<br />
Method<br />
T. Imamura, Japan<br />
<strong>Aerospace</strong> Exploration<br />
Agency, Chofu, Japan<br />
1500<br />
<strong>AIAA</strong>-2007-0230<br />
Aeroacoustic<br />
Comparison of Airfoil<br />
Leading Edge High- Lift<br />
Geometries <strong>and</strong><br />
Supports<br />
C. Andreou, Cambridge<br />
University, Cambridge,<br />
Great Britain<br />
1530<br />
<strong>AIAA</strong>-2007-0231<br />
L<strong>and</strong>ing Gear for a<br />
Silent Aircraft<br />
A. Quayle, University of<br />
Cambridge, Cambridge,<br />
Great Britain<br />
1100<br />
<strong>AIAA</strong>-2007-0217<br />
3D Navier- Stokes<br />
Simulations of a Rotor<br />
Designed for Maximum<br />
Aerodynamic Efficiency<br />
J. Johansen, Risø<br />
National Laboratory,<br />
Roskilde, Denmark<br />
Session 32-ABP-3 PDE <strong>and</strong> Unsteady Flows I Cascade 2<br />
Chaired by: T. KAEMMING, The Boeing Company, Florissant, MO, <strong>and</strong> A. RASHEED, General Electric Global Research Center, Niskayuna, NY<br />
1330<br />
<strong>AIAA</strong>-2007-0232<br />
Simultaneous Mid- IR<br />
Measurement of<br />
Equivalence Ratio <strong>and</strong><br />
Temperature in a JP-<br />
10- Fueled Pulsed<br />
Detonation Engine<br />
E. Barbour, High<br />
Temperature<br />
Gasdynamics<br />
Laboratory Department<br />
of Mechanical<br />
Engineering Stanford<br />
University, Stanford, CA<br />
1400<br />
<strong>AIAA</strong>-2007-0233<br />
Design, Modeling <strong>and</strong><br />
Evaluation of an Initiator<br />
Unit for a Split- Path JP-<br />
10/Air Pulse Detonation<br />
Combustor<br />
P. Hutcheson, Canadian<br />
Air Force, Monterey, CA<br />
1430<br />
<strong>AIAA</strong>-2007-0234<br />
Ignition <strong>and</strong> Detonation-<br />
Initiation Characteristics<br />
of Hydrogen <strong>and</strong><br />
Hydrocarbon Fuels in a<br />
PDE<br />
T. Helfrich, U.S. Air<br />
Force Research<br />
Laboratory,<br />
Wright-Patterson AFB,<br />
OH<br />
1500<br />
<strong>AIAA</strong>-2007-0235<br />
Evaluation of Catalytic<br />
<strong>and</strong> Thermal Cracking in<br />
a JP- 8 Fueled Pulsed<br />
Detonation Engine<br />
T. Helfrich, U.S. Air<br />
Force Research<br />
Laboratory,<br />
Wright-Patterson AFB,<br />
OH<br />
1530<br />
<strong>AIAA</strong>-2007-0236<br />
IGNITION AND<br />
DETONATION<br />
INITIATION OF<br />
MOVING HYDROGEN-<br />
AIR MIXTURES AT<br />
ELEVATED<br />
TEMPERATURE AND<br />
PRESSURE<br />
D. Chapin, GE Global<br />
Research Center,<br />
Niskayuna, NY<br />
1600<br />
<strong>AIAA</strong>-2007-0237<br />
Development of a<br />
Compact Liquid Fueled<br />
PDE with Predetonator<br />
P. Panicker, University<br />
of Texas at Arlington,<br />
Arlington, TX<br />
1630<br />
<strong>AIAA</strong>-2007-0238<br />
Experimental Study of<br />
Kerosene- Fueled Pulse<br />
Detonation Rocket<br />
Engine<br />
Q. Li, Northwestern<br />
Polytechnical University,<br />
Xi'an, China (prc)
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