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  • LUNAR AND PLANETARY EXPLORATION  (601)
  • AERODYNAMICS  (366)
  • SPACE SCIENCES
  • 1980-1984  (967)
  • 1955-1959
  • 1945-1949
  • 1981  (967)
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  • 1980-1984  (967)
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  • 1
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    Current developments lighter than air systems (1981)
    In:  CASI
    Details
    Publikationsdatum: 2019-08-28
    Beschreibung: Lighter than air aircraft (LTA) developments and research in the United States and other countries are reviewed. The emphasis in the U.S. is on VTOL airships capable of heavy lift, and on long endurance types for coastal maritime patrol. Design concepts include hybrids which combine heavier than air and LTA components and characteristics. Research programs are concentrated on aerodynamics, flight dynamics, and control of hybrid types.
    Schlagwort(e): AERODYNAMICS
    Materialart: NASA-TM-84744 , NAS 1.15:84744
    Format: application/pdf
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  • 2
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    The Viking seismometry (1981)
    In:  CASI
    Details
    Publikationsdatum: 2019-08-28
    Beschreibung: Efforts were made to determine the seismicity of Mars as well as define its internal structure by detecting vibrations generated by marsquakes and meteoroid impacts. The lack of marsquakes recognized in the Viking data made it impossible to make any direct inferences about the interior of Mars and only allowed the setting of upper bounds on the seismic activity of the planet. After obtaining more than 2100 hours worth of data during the quite periods at rates of one sample per second or higher, the Viking 2 seismometer was turned off as a consequence of a landing system failure. During the periods when adequate data were obtained, one event of possible seismic or meteoroid impact origin was recognized; however, there is a significant probability that this event was generated by a wind gust.
    Schlagwort(e): LUNAR AND PLANETARY EXPLORATION
    Materialart: NASA-CR-3408
    Format: application/pdf
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  • 3
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    Experimental investigation of the flow on the suction side of a thin Delta wing (1981)
    In:  CASI
    Details
    Publikationsdatum: 2019-08-28
    Beschreibung: Surface oil flow patterns were photographed and pressure distribution measurements were carried out on a sharp edged delta wing of aspect ratio lambda = 1.0 in order to determine the influence of Reynolds number and of vortex breakdown on the flow on the suction side of the wing. The formation of the secondary vortex occurs due to separation of a laminar boundary layer in the front part of the wing and due to separation of a turbulent boundary layer in the rear part of the wing. In the case of turbulent separation, the secondary separation line is closer to the wing leading edge than in the laminar case. The position of the transition depends on the Reynolds number and on the angle of incidence. The breakdown of a vortex above the wing leads to a kink in the secondary separation line.
    Schlagwort(e): AERODYNAMICS
    Materialart: NASA-TM-75897
    Format: application/pdf
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  • 4
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    Thermal inertia mapping of Mars from 60 deg S to 60 deg N (1981)
    In:  Other Sources
    Details
    Publikationsdatum: 2019-08-28
    Beschreibung: The considered region comprises 81% of the surface of Mars. Thermal inertia I is a composite surface property, which is equal to the square root of the product of three factors, including the thermal conductivity, the density, and the specific heat. I is the sole thermal parameter which governs the temperature variation of a periodically heated homogeneous surface, and, as such, is the prime intermediary between remote temperature observations and their geologic interpretation. The values for the thermal inertia found imply particulate surface materials. The variation in Martian surface thermal conductivity is about two orders of magnitude. Three large regions of low-inertia material are defined. Low-inertia material always possesses high albedo. There is a general tendency for higher-thermal-inertia surfaces to be darker but exceptions occur which may be related to a thin mantling of light dust or bonding of light material.
    Schlagwort(e): LUNAR AND PLANETARY EXPLORATION
    Materialart: Icarus; 45; Feb. 198
    Format: text
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  • 5
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    Separation behavior of boundary layers on three-dimensional wings (1981)
    In:  CASI
    Details
    Publikationsdatum: 2019-08-28
    Beschreibung: An inverse boundary layer procedure for calculating separated, turbulent boundary layers at infinitely long, crabbing wing was developed. The procedure was developed for calculating three dimensional, incompressible turbulent boundary layers was expanded to adiabatic, compressible flows. Example calculations with transsonic wings were made including viscose effects. In this case an approximated calculation method described for areas of separated, turbulent boundary layers, permitting calculation of this displacement thickness. The laminar boundary layer development was calculated with inclined ellipsoids.
    Schlagwort(e): AERODYNAMICS
    Materialart: NASA-TM-75877
    Format: application/pdf
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  • 6
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    Press conference on Voyager 2 Saturn encounter (1981)
    In:  CASI
    Details
    Publikationsdatum: 2019-08-28
    Schlagwort(e): LUNAR AND PLANETARY EXPLORATION
    Materialart: P81-10211
    Format: text
    Standort Signatur Erwartet Verfügbarkeit
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  • 7
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    Advances in planetary geology (1981)
    In:  CASI
    Details
    Publikationsdatum: 2019-08-28
    Beschreibung: This second issue in a new series intended to serve the planetary geology community with a form for quick and thorough communications includes (1) a catalog of terrestrial craterform structures for northern Europe; (2) abstracts of results of the Planetary Geology Program, and (3) a list of the photographic holdings of regional planetary image facilities.
    Schlagwort(e): LUNAR AND PLANETARY EXPLORATION
    Materialart: NASA-TM-83089
    Format: application/pdf
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  • 8
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    Highly separated transonic flows (1981)
    In:  CASI
    Details
    Publikationsdatum: 2019-08-28
    Beschreibung: Attention is given to the wind tunnel, to photographic visualization of the flow, and to measurements by pressure probes, hot wire anemometry and laser anemometry. The simultaneous use of different means of measurement provided a good description of the phenomenon, and indicated the existence of shocks and their stability, as well as the existence of the bubble, its dimensions, and in particular, the reattachment of its front. The results show that the bursting (or transition) of the bubble front is produced at an unstable position and creates a point of turbulent intensity which diffuses over the entire height of the flow.
    Schlagwort(e): AERODYNAMICS
    Materialart: NASA-TM-75874 , NT80-18 , Colloq. Aerodyn. Appl.; Nov 13, 1979 - Nov 15, 1979; Lille; France
    Format: application/pdf
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  • 9
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    Experimental investigation of a transonic potential flow around a symmetric airfoil (1981)
    In:  CASI
    Details
    Publikationsdatum: 2019-08-27
    Beschreibung: Experimental flow investigations on smooth airfoils were done using numerical solutions for transonic airfoil streaming with shockless supersonic range. The experimental flow reproduced essential sections of the theoretically computed frictionless solution. Agreement is better in the expansion part of the of the flow than in the compression part. The flow was nearly stationary in the entire velocity range investigated.
    Schlagwort(e): AERODYNAMICS
    Materialart: NASA-TM-76676 , REPT-10/1971
    Format: application/pdf
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  • 10
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    Voyager backgrounder (1981)
    In:  CASI
    Details
    Publikationsdatum: 2019-08-27
    Beschreibung: The Voyager spacecraft and experiments are described. The spacecraft description includes the structure and configuration, communications systems, power supplies, computer command subsystems, and the science platform. The experiments discussed are investigations of cosmic rays, low-energy charged particles, magnetic fields, and plasma waves, along with studies in radio astronomy photopolarimetry. The tracking and data acquisition procedures for the missions are presented.
    Schlagwort(e): LUNAR AND PLANETARY EXPLORATION
    Materialart: NASA-NEWS-RELEASE-81-116 , P81-10118
    Format: application/pdf
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