ALBERT

All Library Books, journals and Electronic Records Telegrafenberg

X
feed icon rss

Your email was sent successfully. Check your inbox.

An error occurred while sending the email. Please try again.

Proceed reservation?

Export
  • 1
    facet.materialart.
    Unknown
    Planetary entry aerothermodynamics. II - Computational analyses and flight experience (1974)
    In:  Other Sources
    Details
    Publication Date: 2011-08-16
    Description: Limitations concerning the possibility to simulate all the significant flow and thermal phenomena occurring during the entry of a space vehicle into a planetary atmosphere make it necessary to rely on computational analyses to obtain the required data for the design of the spacecraft needed for the NASA missions planned for the next two decades. 'Benchmark' computer programs concerned with complete, detailed, and accurate computational solutions of entry problems are considered along with programs representing engineering approximations for cases in which the accuracy provided by the benchmark programs is not needed. The information obtainable by computational analysis has to be supplemented by actual flight experience in order to meet the goals of the NASA entry-technology program. The individual space missions planned for the coming years are examined together with the possibilities for obtaining the data needed to satisfy the entry requirements in each case.
    Keywords: AERODYNAMICS
    Type: Astronautics and Aeronautics; 12; Dec. 197
    Format: text
    Location Call Number Expected Availability
    BibTip Others were also interested in ...
    NASA TECHNICAL REPORTS
  • 2
    facet.materialart.
    Unknown
    Effects of vertical-tail size and a ventral fin on the static lateral and directional stability derivatives of a 0.048-scale model of a horizontal-attitude VTOL airplane at transonic speeds (1960)
    In:  CASI
    Details
    Publication Date: 2019-05-29
    Description: Vertical tail size and ventral fin effects on lateral and directional stability of VTOL AIRCRAFT at transonic speeds
    Keywords: AERODYNAMICS
    Type: NASA-TM-X-35
    Format: application/pdf
    Location Call Number Expected Availability
    BibTip Others were also interested in ...
    NASA TECHNICAL REPORTS
  • 3
    facet.materialart.
    Unknown
    Aerodynamic characteristics in pitch, including effects of horizontal-tail negative dihedral angle, of a 0.048-scale model of a horizontal-attitude VTOL airplane at transonic speeds (1960)
    In:  CASI
    Details
    Publication Date: 2019-05-29
    Description: Aerodynamic characteristics in pitch of horizontal attitude VTOL aircraft, including effects of negative dihedral horizontal tail
    Keywords: AERODYNAMICS
    Type: NASA-TM-X-11
    Format: application/pdf
    Location Call Number Expected Availability
    BibTip Others were also interested in ...
    NASA TECHNICAL REPORTS
  • 4
    facet.materialart.
    Unknown
    An approximate inviscid radiating flow field analysis for outer planet entry probes (1978)
    In:  Other Sources
    Details
    Publication Date: 2019-07-13
    Description: An approximate computational technique has been developed for predicting inviscid, radiating flows about blunt probes entering atmospheres consisting of hydrogen and helium. The technique is rapid and versatile and is well suited for performing parametric trade studies for outer planet entries. Details of the computational technique, the thermodynamic correlations, the 58-step absorption coefficient model and the analytic shock shape equations are discussed. Good comparisons of the radiative heating computed by the approximate method and by detailed calculations are obtained.
    Keywords: AERODYNAMICS
    Type: AIAA PAPER 78-189 , Aerospace Sciences Meeting; Jan 16, 1978 - Jan 18, 1978; Huntsville, AL
    Format: text
    Location Call Number Expected Availability
    BibTip Others were also interested in ...
    NASA TECHNICAL REPORTS
  • 5
    facet.materialart.
    Unknown
    Entry heating and thermal protection (1980)
    In:  Other Sources
    Details
    Publication Date: 2019-08-13
    Description: The book provides a documentation of progress in entry heating and thermal protection as related to two very challenging and very dissimilar applications, viz., the Jovian atmospheric probe as a key element of the Galileo mission, and the Space Shuttle. The Jovian atmospheric probe presents what might be the ultimate challenge in terms of the severity of entry. Success of the Galileo probe depends upon a design based on computational analysis largely unverified by experiment. Topics of interest include methods for predicting off-stagnation-point flowfields for planetary entry probes, modeling of radiative heating in base region of Jovian entry probe, gas heating with pressure gradients for the Space Shuttle, external tank laminar and rarefied aeroheating, and a study of the aerothermal entry environment for the Galileo probe.
    Keywords: AERODYNAMICS
    Format: text
    Location Call Number Expected Availability
    BibTip Others were also interested in ...
    NASA TECHNICAL REPORTS
  • 6
    facet.materialart.
    Unknown
    Nongray radiating flow about smooth symmetric bodies with large blowing. (1969)
    In:  Other Sources
    Details
    Publication Date: 2019-07-13
    Description: Nongray absorption and radiation cooling on smooth symmetric blunt bodies included in modified Maslen flow field method for radiation and large blowing
    Keywords: AERODYNAMICS
    Type: AIAA PAPER 69-637 , AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, THERMOPHYSICS CONFERENCE; Jun 16, 1969 - Jun 18, 1969; SAN FRANCISCO, CALIF.
    Format: text
    Location Call Number Expected Availability
    BibTip Others were also interested in ...
    NASA TECHNICAL REPORTS
  • 7
    facet.materialart.
    Unknown
    Nongray radiating flow about smooth symmetric bodies (1971)
    In:  Other Sources
    Details
    Publication Date: 2019-07-13
    Description: Nongray absorption and radiation cooling on smooth symmetric blunt bodies included in modified Maslen flow field method for radiation and large blowing
    Keywords: AERODYNAMICS
    Type: AIAA PAPER 69-637 , THERMOPHYSICS CONFERENCE; Jun 16, 1969 - Jun 18, 1969; SAN FRANCISCO, CA|; BROTECHNIKA, NO. 2(
    Format: text
    Location Call Number Expected Availability
    BibTip Others were also interested in ...
    NASA TECHNICAL REPORTS
Close ⊗
This website uses cookies and the analysis tool Matomo. More information can be found here...