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Subject: "To 70"
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T - Technology
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B-70 bomber

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1.
Flight investigation of a structural mode control system for the XB-70 aircraft
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973.
Location
Library Shelving Facility (LSF) >> NASA TN D-7420
Format
Books
2.
Flight investigation of XB-70 structural response to oscillatory aerodynamic shaker excitation and correlation with analytical results
Author
McKay, James M.
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973.
Location
Library Shelving Facility (LSF) >> NASA TN D-7227
Format
Books
3.
Flight-measured base pressure coefficients for thick boundary-layer flow over an aft-facing step for Mach numbers from 0.4 to 2.5
Author
Goecke, Sheryll A.
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973.
Location
Library Shelving Facility (LSF) >> NASA TN D-7202
Format
Books
4.
Measurements of surface-pressure fluctuations on the XB-70 airplane at local Mach numbers up to 2.45
Author
Lewis, Thomas L.
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973.
Location
Library Shelving Facility (LSF) >> NASA TN D-7226
Format
Books
5.
Local skin friction coefficients and boundary-layer profiles obtained in flight from the XB-70-1 airplane at Mach numbers up to 2.5
Author
Fisher, David F.
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973.
Location
Library Shelving Facility (LSF) >> NASA TN D-7220
Format
Books