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  • Aerodynamics
  • Aircraft Stability and Control
  • 2020-2024
  • 1995-1999
  • 1960-1964  (3)
  • 1945-1949
  • 1964  (3)
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Schlagwörter
Erscheinungszeitraum
  • 2020-2024
  • 1995-1999
  • 1960-1964  (3)
  • 1945-1949
Jahr
  • 1
    facet.materialart.
    Unbekannt
    Spin-Tunnel Investigation of a 1/30-Scale Model of the North American A-5 Airplane (1964)
    In:  CASI
    Details
    Publikationsdatum: 2019-08-24
    Beschreibung: An investigation has been made to determine the erect and. inverted spin and recovery characteristics of a 1/30-scale dynamic model of the North American A-5A airplane. Tests were made for the basic flight design loading with the center of gravity at 30-percent mean aerodynamic chord and also for a forward position and a rearward position with the center of gravity at 26-percent and 40-percent mean aerodynamic chord, respectively. Tests were also made to determine the effect of full external wing tanks on both wings, and of an asymmetrical condition when only one full tank is carried.
    Schlagwort(e): Aircraft Stability and Control
    Materialart: NASA-TM-SX-946 , NACA-AD-3140 , L-3663
    Format: application/pdf
    Standort Signatur Erwartet Verfügbarkeit
    BibTip Andere fanden auch interessant ...
    NASA TECHNICAL REPORTS
  • 2
    facet.materialart.
    Unbekannt
    Spin Tunnel Investigation of a 1/30 Scale Model of the North American A-5A Airplane (1964)
    In:  CASI
    Details
    Publikationsdatum: 2019-08-15
    Beschreibung: An investigation has been made in the Langley spin tunnel to determine the erect and inverted spin and recovery characteristics of a 1/30-scale dynamic model of the North American A-5A airplane. Tests were made for the basic flight design loading with the center of gravity at 30-percent mean aerodynamic chord and also for a forward position and a rearward position with the center of gravity at 26-percent and 40-percent mean aerodynamic chord, respectively. Tests were also made to determine the effect of full external wing tanks on both wings, and of an asymmetrical condition when only one full tank is carried.
    Schlagwort(e): Aircraft Stability and Control
    Materialart: NASA-TM-SX-946 , NACA-AD-3140 , L-3663
    Format: application/pdf
    Standort Signatur Erwartet Verfügbarkeit
    BibTip Andere fanden auch interessant ...
    NASA TECHNICAL REPORTS
  • 3
    facet.materialart.
    Unbekannt
    On the Mechanics of Transition Produced by Particles Passing Through an Initially Laminar Boundary Layer and the Estimated Effect on the LFC Performance of the X-21 Aircraft (1964)
    In:  CASI
    Details
    Publikationsdatum: 2019-08-14
    Beschreibung: Numerous flight tests of the X-21 aircraft have shown total loss of LFC while flying within, or in the proximity of, visible clouds. In addition, erratic LFC performance has been observed in conditions of light haze when the humidity of the air is relatively high. An investigation of the phenomena which might account for loss of LFC in or near clouds and for the erratic performance in light haze has been conducted. The phenomena considered in the investigation are classified as either thermodynamic effects or mechanical effects. The results derived from the study of thermodynamic and mechanical effects are presented with recommendations for follow-up work.
    Schlagwort(e): Aerodynamics
    Materialart: HQ-E-DAA-TN42874
    Format: application/pdf
    Standort Signatur Erwartet Verfügbarkeit
    BibTip Andere fanden auch interessant ...
    NASA TECHNICAL REPORTS
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