NASA NTRS · 19660010176
An empirical method for determining static distributed aerodynamic loads on axisymmetric multistage launch vehicles
Abstract
Empirical method for determining static distributed aerodynamic loads on axisymmetric multistage launch vehicles
Explore related subjects
Keep this discovery
Explore connections, maps & timelines
Muraca, R. J.. 1966-03-01. An empirical method for determining static distributed aerodynamic loads on axisymmetric multistage launch vehicles. https://ntrs.nasa.gov/citations/19660010176
Cite the original work for its findings. Save a collection to share your selection of sources.