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  • RESEARCH AND SUPPORT FACILITIES (AIR)  (1)
  • THERMODYNAMICS AND COMBUSTION  (1)
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  • 1
    facet.materialart.
    Unknown
    Design of static reaction gantry for an ultralight airplane destruction test (1985)
    In:  Other Sources
    Details
    Publication Date: 2019-06-28
    Description: The steel gantry superstructure needed to perform an airplane static test is described. Standard civil engineering design practices are used to react the loads generated by an airplane in flight. Reaction columns are mounted on a structural floor to carry the wing airloads and the downward acting fuselage loads are carried directly into the floor. The gantry can accommodate a general aviation airplane or rotorcraft. An immediate use for an ultralight airplane is shown as an example configuration of the four main steel frames.
    Keywords: RESEARCH AND SUPPORT FACILITIES (AIR)
    Type: AIAA PAPER 85-4022
    Format: text
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    NASA TECHNICAL REPORTS
  • 2
    facet.materialart.
    Unknown
    Combustion of a premixed system in stagnation flow. I - Theoretical. (1971)
    In:  Other Sources
    Details
    Publication Date: 2019-06-27
    Description: The theoretical steady-state and transient characteristics of a premixed combustible system in laminar axisymmetric stagnation flow are studied by way of numerical solution of the governing boundary-layer equations. Computations, which are based on the oxidation reaction of carbon monoxide in humid air, invoke a minimum of simplifying assumptions. Steady-state results include prediction of (1) profiles of the state variables, (2) extinction of blow-off conditions, (3) ignition conditions, and (4) the heat flux to the stagnation point. Computer simulations of the unsteady state provide an indication of the stability of a given steady state to perturbations. Comparisons between some of the predictions of the mathematical model and the results of laboratory experiments will be reported in Part II.
    Keywords: THERMODYNAMICS AND COMBUSTION
    Type: AD-743387 , AROD-5648-8-E , Combustion Science and Technology; 4; Nov. 197
    Format: text
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    NASA TECHNICAL REPORTS
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