Max. A. Heaslet

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Books

An Analysis of the Stability and Ultimate Compressive Strength of Short Sheet-stringer Panels with Special Reference to the Influence of the Riveted Connection Between Sheet and Stringer

An Analysis of the Stability and Ultimate Compressive Strength of Short Sheet-stringer Panels with Special Reference to the Influence of the Riveted Connection Between Sheet and Stringer

United States. National Advisory Committee for Aeronautics, Robert J. Tapscott, John B. McDevitt, Max. A. Heaslet, Benjamin H. Beam, Dean R. Chapman, Joseph W. Semonian, Franklin B. Fuller, James P. Peterson, Julian H. Berman, Kenneth B. Amer

Method for Calculation of Laminar Heat Transfer in Air Flow Around Cylinders of Arbitrary Cross Section (including Large Temperature Differences and Transpiration Cooling)

Method for Calculation of Laminar Heat Transfer in Air Flow Around Cylinders of Arbitrary Cross Section (including Large Temperature Differences and Transpiration Cooling)

United States. National Advisory Committee for Aeronautics, Max. A. Heaslet, John D. Stanitz, Dwight G. Moore, E. R. G. Eckert, H. S. Ribner, Herbert F. Hardrath, Simon Ostrach

Investigation of the Drag of Various Axially Symmetric Nose Shapes of Fineness Ratio 3 for Mach Numbers from 1.24 to 7.4

Investigation of the Drag of Various Axially Symmetric Nose Shapes of Fineness Ratio 3 for Mach Numbers from 1.24 to 7.4

United States. National Advisory Committee for Aeronautics, Franklyn B. Fuller, Edmund E. Callaghan, Willard D. Coles, Ray H. Wright, C. H. Wilts, Edward W. Perkins, Isadore L. Drell, Lewis Laboratory Staff, Max. A. Heaslet, Frank E. Belles, Leland H. Jorgensen, Virgil S. Ritchie, Albin O. Pearson, Simon C. Sommer

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