naca-rm-l56b21
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- October 13, 2017 Create Date
- October 13, 2017 Last Updated
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Wind Tunnel Investigation of a Ram Jet Missile Model having a Wing and Canard Surfaces of Delta Plan Form with 70° Swept Leading Edges
Force and Moment Characteristics at Combined Angles of Pitch and Sideslip for Mach Number 2.01
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naca-rm-l56b21 Wind Tunnel Investigation of a Ram Jet Missile Model having a Wing and Canard Surfaces of Delta Plan Form with 70° Swept Leading Edges.pdf | Download |
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