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 Afternoon / 08 January 2007<br />
Session 33-AD-2 Launch Vehicle <strong>and</strong> Spacecraft Design Crystal 3<br />
Chaired by: R. CURRAN, Queen's University, Belfast, Northern Irel<strong>and</strong><br />
1330<br />
<strong>AIAA</strong>-2007-0240<br />
Benefits From<br />
Incorporation of<br />
Combined Cycle<br />
Propulsion: X- 33<br />
Revisited<br />
P. Czysz, HyperTech<br />
Concepts LLC, St.<br />
Louis, MO<br />
1400<br />
<strong>AIAA</strong>-2007-0241<br />
Overview of a HTHL<br />
H<strong>and</strong>s- On SAV Design<br />
Synthesis Methodology<br />
X. Huang, University of<br />
Oklahoma, Norman, OK<br />
Monday Afternoon / 08 January 2007<br />
Session 34-AFM-2 Air Vehicle Dynamics <strong>and</strong> Flight Mechanics N-11<br />
Monday Afternoon / 08 January 2007<br />
1430<br />
<strong>AIAA</strong>-2007-0242<br />
Application of a HTHL<br />
SAV Design<br />
Methodology to<br />
Suborbital Tourism<br />
Vehicle<br />
X. Huang, University of<br />
Oklahoma, Norman, OK<br />
1500<br />
<strong>AIAA</strong>-2007-0243<br />
Flight Testing <strong>and</strong><br />
Simulation of a Mars<br />
Aircraft Design Using<br />
Inflatable Wings<br />
D. Reasor, University of<br />
Kentucky, Lexington, KY<br />
1530<br />
<strong>AIAA</strong>-2007-0244<br />
Mars Intelligent<br />
Reconaissance Aerial<br />
<strong>and</strong> Ground Explorer<br />
(MIRAGE)<br />
J. Aguirre, University of<br />
Miami, Coral Gables, FL<br />
Chaired by: G. SHAH, NASA Langley Research Center, Hampton, VA, <strong>and</strong> R. HESS, University of California, Davis, Davis, CA<br />
1330<br />
<strong>AIAA</strong>-2007-0247<br />
Obtaining Multi- Loop<br />
Pursuit- Control Pilot<br />
Models From Computer<br />
Simulation<br />
R. Hess, Dept. of<br />
Mechanical <strong>and</strong><br />
Aeronautical<br />
Engineering University<br />
of California , Davis, CA<br />
1400<br />
<strong>AIAA</strong>-2007-0248<br />
High- Order Dynamic<br />
Overset Procedure<br />
Applied to Moving Body<br />
Calculations<br />
K. Alabi, Thaerocomp<br />
Technical Corp., Stony<br />
Brook, NY<br />
1430<br />
<strong>AIAA</strong>-2007-0249<br />
The Application of<br />
Quaternion Algebra to<br />
Gyroscopic Motion,<br />
Navigation, <strong>and</strong><br />
Guidance<br />
G. Davailus, Old<br />
Dominion University,<br />
Norfolk, VA<br />
1500<br />
<strong>AIAA</strong>-2007-0250<br />
Formation Flying<br />
Commercial Aircraft -<br />
Assessment Using a<br />
New Approach - Wing<br />
Span Load <strong>and</strong> Camber<br />
Control<br />
R. Nangia, Nangia Aero<br />
Research, Bristol, Great<br />
Britain<br />
1530<br />
<strong>AIAA</strong>-2007-0251<br />
Derivation of the<br />
Dynamics Equations of<br />
Receiver Aircraft in<br />
Aerial Refueling<br />
J. Tucker, University of<br />
Texas at Arlington,<br />
Arlington, TX<br />
1600<br />
<strong>AIAA</strong>-2007-0252<br />
Optimal Turn- Back<br />
Maneuver After Engine<br />
Failure in a Single-<br />
Engine Aircraft During<br />
Climb- Out<br />
K. Brinkman, Delft<br />
University of<br />
Technology, Delft, The<br />
Netherl<strong>and</strong>s<br />
1630<br />
<strong>AIAA</strong>-2007-0253<br />
A Closed- Loop<br />
Guidance Approximation<br />
for the Turn- Back<br />
Maneuver After Engine<br />
Failure During Climb-<br />
Out<br />
K. Brinkman, Delft<br />
University of<br />
Technology, Delft, The<br />
Netherl<strong>and</strong>s<br />
Session 35-APA-4 Drag Prediction Workshop Summary Carson 1<br />
Chaired by: R. WAHLS, NASA Langley Research Center, Hampton, VA, <strong>and</strong> R. RUDNIK, DLR, German <strong>Aerospace</strong> Research Center, Brunswick, Germany<br />
1330<br />
<strong>AIAA</strong>-2007-0260<br />
Summary of the Third<br />
<strong>AIAA</strong> CFD Drag<br />
Prediction Workshop<br />
J. Vassberg, The Boeing<br />
Company, Huntington<br />
Beach, CA<br />
1400<br />
<strong>AIAA</strong>-2007-0254<br />
Statistical Analysis of<br />
CFD Solutions from the<br />
Third <strong>AIAA</strong> Drag<br />
Prediction Workshop<br />
(Invited)<br />
J. Morrison, NASA<br />
Langley Research<br />
Center, Hampton, VA<br />
1430<br />
<strong>AIAA</strong>-2007-0255<br />
Structured <strong>and</strong><br />
Unstructured Solvers for<br />
the 3rd CFD Drag<br />
Prediction Workshop<br />
(Invited)<br />
E. Tinoco, The Boeing<br />
Company, Seattle, WA<br />
1500<br />
<strong>AIAA</strong>-2007-0256<br />
Results from the 3rd<br />
Drag Prediction<br />
Workshop Using the<br />
NSU3D Unstructured<br />
Mesh Solver<br />
D. Mavriplis, University<br />
of Wyoming, Laramie,<br />
WY<br />
1530<br />
<strong>AIAA</strong>-2007-0257<br />
Drag Prediction for the<br />
DLR- F6 Wing/Body <strong>and</strong><br />
DPW Wing Using<br />
CFL3D <strong>and</strong><br />
OVERFLOW on an<br />
Overset Mesh<br />
A. Sclafani, The Boeing<br />
Company, Huntington<br />
Beach, CA<br />
1600<br />
<strong>AIAA</strong>-2007-0258<br />
Comparison Study of<br />
Drag Prediction for the<br />
3rd CFD Drag<br />
Prediction Workshop by<br />
Structured <strong>and</strong><br />
Unstructured Mesh<br />
Method (Invited)<br />
M. Murayama, Japan<br />
<strong>Aerospace</strong> Exploration<br />
Agency, Chofu, Japan<br />
1630<br />
<strong>AIAA</strong>-2007-0259<br />
DLR Results from the<br />
Third <strong>AIAA</strong> CFD Drag<br />
Prediction Workshop<br />
(Invited)<br />
O. Brodersen, DLR,<br />
Institute of<br />
Aerodynamics <strong>and</strong> Flow<br />
Technology,<br />
Braunschweig, Germany
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