Back to Results
First PageMeta Content
Aerodynamics / Plume / Shock wave / Bow shock / Aerodynamic drag / Mach number / Nozzle / Oblique shock / Lift / Fluid dynamics / Fluid mechanics / Dynamics


AIAA[removed]AIAA SciTech[removed]January 2014, National Harbor, Maryland AIAA Atmospheric Flight Mechanics Conference An Analytical Approach to Modeling Supersonic
Add to Reading List

Document Date: 2014-01-25 15:05:06

Open Document

File Size: 1,71 MB

Share Result on Facebook

Company

Astronautics Inc. / /

Facility

Wind tunnel / Robert D. Braun2 Georgia Institute of Technology / American Institute of Aeronautics / National Harbor / A. Bow Shock Shape Equations Van Dyke / Van Dyke / /

IndustryTerm

potential deceleration technology / /

Organization

Georgia Institute of Technology / Atlanta / Guggenheim School of Aerospace Engineering / American Institute of Aeronautics / /

Person

David / Christopher E. Cordell Jr. / Ai / Robert D. Braun / /

Position

oblique shock cascade forward / driver / representative / Associate Professor of Space Technology / forward / constant Graduate Research Assistant / model for multiple SRP configurations / /

ProvinceOrState

Georgia / /

Technology

fluid dynamics / potential deceleration technology / /

URL

http /

SocialTag