Books by "Max. A. Heaslet"

5 books found

The spanwise and chordwise distribution of loading, the lift, and the induced drag of a swept-back wing of slender plan form are developed by means of linearized lifting-surface theory. The results are applicable for all free-stream Mach numbers. The term slender implies that the ratio of the reduced span to over-all length of the wing is small.

Cooperative Investigation of Relationship Between Static and Fatigue Properties of Wrought N-155 Alloy at Elevated Temperatures

Cooperative Investigation of Relationship Between Static and Fatigue Properties of Wrought N-155 Alloy at Elevated Temperatures

by Clyde C. Swett, G. B. Schubauer, H. B. Tolefson, Harvard Lomax, Naca Subcommittee on Power-Plant Materials, R. I. Sears, Robert R. McCready, Robert T. Jones, William R. Mickelsen, United States. National Advisory Committee for Aeronautics, C. F. Merlet, Max. A. Heaslet, Norman E. Ernstein, P. S. Klebanoff, L. W. Putland

1956

Use of Source Distributions for Evaluating Theoretical Aerodynamics of Thin Finite Wings at Supersonic Speeds

Use of Source Distributions for Evaluating Theoretical Aerodynamics of Thin Finite Wings at Supersonic Speeds

by A. J. Eggers, Arthur W. Goldstein, Chung-Hua Wu, Dean R. Chapman, George J. Heimerl, Harvard Lomax, John C. Evvard, John D. Stanitz, Max. A. Heaslet, S. S. Manson, United States. National Advisory Committee for Aeronautics, Artur Mager, Gaylord O. Ellis, Lincoln Wolfestein, Loma Sluder, William M. Roberts, John R. Spreiter

1950

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

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

1958

Torsional Stiffness of Thin-walled Shells Having Reinforcing Cores and Rectangular, Triangular, Or Diamond Cross Section

Torsional Stiffness of Thin-walled Shells Having Reinforcing Cores and Rectangular, Triangular, Or Diamond Cross Section

by Alberta Y. Alksne, George J. Nothwang, Harvey G. McComb, Henry H. Heyson, John H. Povolny, Keith C. Harder, Max A. Heaslet, Mitchel H. Bertram, Rinaldo J. Brun, W. E. Moeckel, United States. National Advisory Committee for Aeronautics, E. B. Klunker, Fred W. Steffen, John R. Spreiter, S. Katzoff, Jack G. McArdle

1957