Showing 1 - 20 results of 84 for search '', query time: 0.19s Refine Results
  1. 1
    A theoretical investigation for delta wings with leading-edge separation at low speeds /
    by Nangia, R. K.
    Published 1970
    Book
  2. 2
    Delta wings with longitudinal camber at low speed /
    by Nangia, R. K.
    Published 1970
    Book
  3. 3
    Wind tunnel tests and theoretical investigations on the effect of a localised mass on the flutter of a delta wind with fixed root /
    by Donno, G. F.
    Published 1962
    Book
  4. 4
    Effects of wing stiffness and inertia changes on the modes and frequencies of a model delta aircraft /
    by Webb, D. R. B.
    Published 1962
    Book
  5. 5
    Experiments on a delta wing with jet-assisted lift /
    by Melbourne, W. H.
    Published 1962
    Book
  6. 6
    Flight measurements of the lift, longitudinal trim and drag of the Fairey Delta 2 at mach numbers up to 1.65 and comparisons with wind-tunnel results /
    by Rose, Robert
    Published 1969
    Book
  7. 7
    The use of conical camber to produce flow attachment at the leading edge of a delta wing and to minimize life-dependent drag at sonic and supersonic speeds /
    by Smith, Jeremy H. B.
    Published 1963
    Book
  8. 8
    Tests at subsonic and supersonic speeds on a slender cambered wing with fin, underwing engine nacelles and trailing-edge controls /
    by Isaacs, Donald
    Published 1969
    Book
  9. 9
    Measurements : at Mach numbers up to 2.8, of the longitudinal characteristics of one plane and three cambered slender 'ogee' wings /
    by Taylor, C. R.
    Published 1963
    Book
  10. 10
    Low-speed wind-tunnel measurements on a thin sharp-edged delta wing with 70 leading-edge sweep : with particular reference to the position of leading-edge-vortex breakdown /
    by Lawford, J. A.
    Published 1963
    Book
  11. 11
    The airforces on the low-aspect-ratio rectangular wing oscillating in sonic flow /
    by Davies, David Eric
    Published 1963
    Book
  12. 12
    Analysis of the static pressure distribution on a Delta wing in subsonic flow /
    by Kirkpatrick, David L. I.
    Published 1970
    Book
  13. 13
    Low-speed wind-tunnel tests on a delta-wing aircraft model (S.R. 177) with blowing over the trailing-edge flaps and ailerons /
    by Butler, S. F. J.
    Published 1966
    Book
  14. 14
    Aileron control of small-aspect-ratio aircraft ; in particular, Delta aircraft /
    by Pinsker, W. J. G.
    Published 1960
    Book
  15. 15
    Some observations of the flow over a deltawinged model with 55-deg leading-edge sweep, at Mach numbers between 04 and 18 /
    by Sutton, E. P.
    Published 1960
    Book
  16. 16
    Low-speed wind-tunnel measurements of the lift, drag and pitching moment on three symmetrical ogee-wing models and on a symmetrical slender wing-body model /
    Book
  17. 17
    Tests on an engine installation for a slender gothic wing at M-1.82 /
    by Griffiths, R. T.
    Published 1967
    Book
  18. 18
    Balance measurements (excluding drag) on a delta wing aircraft at transonic speeds /
    by Shaw, M. M.
    Published 1967
    Book
  19. 19
    Supersonic flutter derivatives for a series of swept and cropped delta wings /
    by Harris, G. Z.
    Published 1967
    Book
  20. 20
    Investigation of the normal force characteristics of slender delta wings with various rhombic cross-sections in subsonic conical flow /
    by Kirkpatrick, David L. I.
    Published 1967
    Book
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