5 books found
by Harvard Lomax, Max A. Heaslet
1949
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.
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
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
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
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