Ballistics Range Boundary-Layer Transition Measurements on Cones at Hypersonic Speeds

Author:

Sheetz Norman W.

Publisher

Springer US

Reference38 articles.

1. Lees, L., “The Stability of the Laminar Boundary Layer in a Compressible Fluid,” NACA Report No. 876, 1947.

2. van Driest, E. R., “Calculation of the Stability of the Laminar Boundary Layer in Compressible Fluid on a Flat Plate with Heat Transfer,” Journal of the Aeronautical Sciences, Vol 19, No. 12, Dec. 1952, pp 801–812

3. van Driest, E. R. y”The Laminary Boundary Layer with Variable Fluid Properties,” Report No. AL-1866, North American Aviation, Inc., Downey, Calif., Jan. 1954

4. Dunn, D. W., and Lin, C. C., “On the Stability of the Laminar Boundary Layer in a Compressible Fluid,” Journal of the Aeronautical Sciences, Vol 22, No. 7, 1955, pp 455–477

5. Higgins, R. W., and Pappas, C. C., “An Experimental Investigation of the Effect of Surface Heating on Boundary-Layer Transition on a Flat Plate in Supersonic Flow,” NACA TN 2351, Apr. 1951

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