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Aerodynamic characteristics of the X-15/B-52 combination
Report presenting an investigation to determine the carry loads and mutual aerodynamic interference effects from high-speed wind-tunnel tests and the drop characteristics of the X-15 through the B-52 flow field from low-speed dynamic-model drop tests and six-degree-of-freedom calculations. The X-15 installation was found to increase drag at cruise conditions by approximately 15 percent.
Date:
1959
Creator:
Alford, William J., Jr. & Taylor, Robert T.
System:
The UNT Digital Library