Showing 1 - 13 results of 13 for search 'Jaquet, Byron M', query time: 0.20s Refine Results
  1. 1
    Aerodynamic characteristics at a mach number of 3.10 of several fourth-stage shapes of the scout research vehicle /
    by Jaquet, Byron M
    Published 1961

    Government Document Book
  2. 2
    Some effects of simulated bending and fourth-stage size on local pressures and normal-force distributions of a model of a scout configuration at a Mach number of 3.10 /
    by Jaquet, Byron M
    Published 1963

    Book
  3. 3
    Effect of linear spanwise variations of twist and circular-arc camber on low-speed static stability, rolling, and yawing characteristics of a 45 degree sweptback wing of aspect ratio 4 and taper ratio 0.6 /
    by Jaquet, Byron M
    Published 1952

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  4. 4
    Wind-tunnel investigation of effects of ground proximity and split flaps on the lateral stability derivatives of a 60 degrees delta-wing model oscillating in yaw /
    by Jaquet, Byron M
    Published 1957

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    Government Document Book
  5. 5
    Effects of fuselage nose length and a canopy on the static longitudinal and lateral stability characteristics of 45 degree sweptback airplane models having fuselages with square cross sections /
    by Jaquet, Byron M
    Published 1957

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    Government Document Book
  6. 6
    Wind-tunnel investigation at low speed of effect of size and position of closed air ducts on static longitudinal and static lateral stability characteristics of unswept-midwing models having wings of aspect ratio 2, 4, and 6 /
    by Jaquet, Byron M
    Published 1955

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  7. 7
    Experimental steady-state yawing deriviatives of a 60 degree delta-wing model as affected by changes in vertical position of the wing and in ratio of fuselage diameter to wing span /
    by Jaquet, Byron M
    Published 1956

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  8. 8
    Investigation of effects of geometric dihedral on low-speed static stability and yawing characteristics of an untapered 45 degrees sweptback-wing model of aspect ratio 2.61 /
    by Queijo, M. J
    Published 1948
    Other Authors: “...Jaquet, Byron M...”

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  9. 9
    A Study of the use of experimental stability derivatives in the calculation of the lateral disturbed motions of a swept-wing airplane and comparison with flight results /
    by Bird, John D
    Published 1950
    Other Authors: “...Jaquet, Byron M...”

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  10. 10
    Calculated effects of geometric dihedral on the low-speed rolling derivatives of swept wings /
    by Queijo, M. J
    Published 1948
    Other Authors: “...Jaquet, Byron M...”

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  11. 11
    Effect of target angular oscillations on pilot-controlled Gemini-Agena docking /
    by Riley, Donald R
    Published 1966
    Other Authors: “...Jaquet, Byron M...”

    Book
  12. 12
    Effect of fuselage and tail surfaces on low-speed yawing characteristics of a swept-wing model as determined in curved-flow test section of Langley stability tunnel /
    by Bird, John D
    Published 1951
    Other Authors: “...Jaquet, Byron M...”

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  13. 13
    Investigation of the influence of fuselage and tail surfaces on low-speed static stability and rolling characteristics of a swept-wing model /
    by Bird, John D
    Published 1952
    Other Authors: “...Jaquet, Byron M...”

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
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