Showing 1 - 20 results of 155 for search '', query time: 0.26s Refine Results
  1. 1
    Visual Computing Environment Workshop /
    Published 1998
    Government Document Conference Proceeding Book
  2. 2
    Airflow /
    by Simons, Martin
    Published 1984
    Book
  3. 3
    Smoke streams ; visualized air flow /
    Book
  4. 4
    Part I: The flow pattern on a tapered swept-back wing at Mach numbers between 0.6 and 1.6. Part II: Experiments with a tapered swept-back wing of Warren 12 planform at Mach numbers between 0.6 and 1.6 /
    by Hall, Ian Murray
    Published 1962
    Book
  5. 5
    Further experimental investigation of the characteristics of cambered gothic wings at Mach numbers from 0.4 to 2.0 /
    by Squire, Leonard Charles
    Published 1963
    Book
  6. 6
    Tip-clearance flow and losses for an isolated compressor blade /
    by Lakshminarayana, B.
    Published 1963
    Book
  7. 7
    A review of research on two-dimensional base flow /
    by Nash, John F.
    Published 1963
    Book
  8. 8
    An analysis of two-dimensional turbulent base flow : including the effect of the approaching boundary layer /
    by Nash, John F.
    Published 1963
    Book
  9. 9
    Conditions for the existence of an inertial subrange in turbulent flow /
    by Bradshaw, P. (Peter), 1935-
    Published 1969
    Book
  10. 10
    Some notes on the flow patterns observed over various swept-back wings at low Mach numbers : (in the R.A.E. 10-ft x 7-ft high speed tunnel) /
    by Haines, A. B.
    Published 1960
    Book
  11. 11
    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
  12. 12
    An analysis of the flow over two 45-deg sweptback wings at high subsonic speeds, and comparison with theory /
    by Cook, R.
    Published 1961
    Book
  13. 13
    The normal impingement of a circular air jet on a flat surface /
    by Bradshaw, P. (Peter), 1935-
    Published 1961
    Book
  14. 14
    Pressure distribution and surface flow on 5% and 9% thick wings with curved tip and 60 sweepback /
    by Garner, Henry Clifford
    Published 1962
    Book
  15. 15
    An investigation of the flow about a plane half-wing of cropped-delta planform and 6 per cent symmetrical section at stream Mach numbers between 0.8 and 1.41 /
    by Rogers, E. W. E.
    Published 1962
    Book
  16. 16
    A discussion of two-dimensional turbulent base flows /
    by Nash, John F.
    Published 1967
    Book
  17. 17
    Flight determination of wing flow patterns and buffet boundaries for the Fairey Delta 2 aircraft at Mach numbers between 0.4 and 1.3 : and comparison with wind tunnel results /
    by Dee, F. W.
    Published 1967
    Book
  18. 18
    Leakage and secondary flows in compressor cascades /
    by Lakshminarayana, B.
    Published 1967
    Book
  19. 19
    The development of a nozzle for absolute airflow measurement by pitot-static traverse /
    by Ascough, John Cecil
    Published 1964
    Book
  20. 20
    The effect of forward speed on the inlet flow distribution and performance of a lifting fan installed in a wing /
    by Gregory, Nigel
    Published 1965
    Book
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