Supersonic wind tunnel tests of two rocket propelled projectile models

Supersonic wind tunnel tests of two rocket propelled projectile models

Two models of rocket propelled projectiles have been tested in the Galcit 2 1/2 inch supersonic wind tunnel at a Mach Number of 3.06, and angles of attack from 0° to 10°. Variations of lift, drag, pitching moment, and position of center pressure with angle of attack have been obtained for each model...

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Bibliographic Details
Main Authors: Fossier, Mike Walter, Small, John
Format: Others
Published: 1947
Online Access:https://thesis.library.caltech.edu/4910/1/Fossier_m_1947.pdf
Fossier, Mike Walter and Small, John (1947) Supersonic wind tunnel tests of two rocket propelled projectile models. Engineer's thesis, California Institute of Technology. doi:10.7907/71EK-W641. https://resolver.caltech.edu/CaltechETD:etd-12092008-082853 <https://resolver.caltech.edu/CaltechETD:etd-12092008-082853>

Internet

https://thesis.library.caltech.edu/4910/1/Fossier_m_1947.pdf
Fossier, Mike Walter and Small, John (1947) Supersonic wind tunnel tests of two rocket propelled projectile models. Engineer's thesis, California Institute of Technology. doi:10.7907/71EK-W641. https://resolver.caltech.edu/CaltechETD:etd-12092008-082853 <https://resolver.caltech.edu/CaltechETD:etd-12092008-082853>

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