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Volumn 2, Issue , 2007, Pages 815-832

Dynamic analysis of atmospheric-entry probes and capsules

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; DATABASE SYSTEMS; DYNAMIC ANALYSIS; SENSITIVITY ANALYSIS; TRAJECTORIES;

EID: 34250849751     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2007-74     Document Type: Conference Paper
Times cited : (25)

References (21)
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    • June
    • Redd, B., Olsen, D. M., and Burton, R. L., "Relationship Between the Aerodynamic Damping Derivatives Measured as a Function of Instantaneous Angular Displacement and the Aerodynamic Damping Derivatives Measured as a Function of Oscillation Amplitude," NASA TN D-2855, June 1965.
    • (1965) NASA TN , vol.D-2855
    • Redd, B.1    Olsen, D.M.2    Burton, R.L.3
  • 2
    • 33748069710 scopus 로고
    • Aerodynamic Stability Characteristics of the Apollo Command Module
    • August
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    • (1968) NASA TN , vol.D-4688
    • Moseley Jr., W.C.1    Graham, R.E.2    Hughes, J.E.3
  • 3
    • 0015650704 scopus 로고
    • Viking Pitch Damping Derivatives as Influenced by Support Interference and Test Techniques
    • July
    • Steinberg, S., Uselton, B.L., and Siemers, III, P.M., "Viking Pitch Damping Derivatives as Influenced by Support Interference and Test Techniques," Journal of Spacecraft and Rockets, 10(7):443-449, July 1973.
    • (1973) Journal of Spacecraft and Rockets , vol.10 , Issue.7 , pp. 443-449
    • Steinberg, S.1    Uselton, B.L.2    Siemers III, P.M.3
  • 8
    • 2942742094 scopus 로고    scopus 로고
    • Implicit Approaches for Moving Boundaries in a 3-D Cartesian Method
    • AIAA Paper 2003-1119, January
    • Murman, S.M., Aftosmis, M.J., and Berger, M.J., "Implicit Approaches for Moving Boundaries in a 3-D Cartesian Method," AIAA Paper 2003-1119, January 2003.
    • (2003)
    • Murman, S.M.1    Aftosmis, M.J.2    Berger, M.J.3
  • 10
    • 30744434681 scopus 로고    scopus 로고
    • Characterization of Space Shuttle Ascent Debris Aerodynamics Using CFD Methods
    • AIAA Paper 2005-1223, January
    • Murman, S.M., Aftosmis, M.J., and Rogers, S.E., "Characterization of Space Shuttle Ascent Debris Aerodynamics Using CFD Methods," AIAA Paper 2005-1223, January 2005.
    • (2005)
    • Murman, S.M.1    Aftosmis, M.J.2    Rogers, S.E.3
  • 12
    • 30744436053 scopus 로고    scopus 로고
    • Dynamic Stability Testing of the Genesis Sample Return Capsule
    • AIAA Paper 2000-1009, January
    • Cheatwood, F.M., Winchenbach, G.L., Hathaway, W., and Chapman, G., "Dynamic Stability Testing of the Genesis Sample Return Capsule," AIAA Paper 2000-1009, January 2000.
    • (2000)
    • Cheatwood, F.M.1    Winchenbach, G.L.2    Hathaway, W.3    Chapman, G.4
  • 15
    • 0032637765 scopus 로고    scopus 로고
    • Entry Dispersion Analysis for the Stardust Comet Sample Return Capsule
    • May
    • Desai, P.N., Mitcheltree, R.A., and Cheatwood, F.M., "Entry Dispersion Analysis for the Stardust Comet Sample Return Capsule," Journal of Spacecraft and Rockets, 36(3): 463-469, May 1999.
    • (1999) Journal of Spacecraft and Rockets , vol.36 , Issue.3 , pp. 463-469
    • Desai, P.N.1    Mitcheltree, R.A.2    Cheatwood, F.M.3
  • 16
    • 0035331465 scopus 로고    scopus 로고
    • Entry Dispersion Analysis for the Genesis Sample Return Capsule
    • May
    • Desai, P.N. and Cheatwood, F.M., "Entry Dispersion Analysis for the Genesis Sample Return Capsule," Journal of Spacecraft and Rockets, 38(3):345-350, May 2001.
    • (2001) Journal of Spacecraft and Rockets , vol.38 , Issue.3 , pp. 345-350
    • Desai, P.N.1    Cheatwood, F.M.2
  • 17
    • 20744460742 scopus 로고    scopus 로고
    • Automated Parameter Studies Using a Cartesian Method
    • AIAA Paper 2004-5076, August
    • Murman, S.M., Aftosmis, M.J., and Nemec, M., "Automated Parameter Studies Using a Cartesian Method," AIAA Paper 2004-5076, August 2004.
    • (2004)
    • Murman, S.M.1    Aftosmis, M.J.2    Nemec, M.3
  • 18
    • 30744459844 scopus 로고    scopus 로고
    • Test Mechanism for Measuring Pitch Damping Derivatives of Missile Configurations at High Angles of Attack
    • AEDC-TR-75-43, May 1975
    • Uselton, B.L. and Uselton, J.C., "Test Mechanism for Measuring Pitch Damping Derivatives of Missile Configurations at High Angles of Attack," AEDC Technical Report AEDC-TR-75-43, May 1975.
    • AEDC Technical Report
    • Uselton, B.L.1    Uselton, J.C.2
  • 19
    • 0013069065 scopus 로고    scopus 로고
    • Dynamic and Static Stability Measurements of the Basic Finner at Supersonic Speeds
    • 4516, September 1960
    • Shantz, I. and Graves, R.T., "Dynamic and Static Stability Measurements of the Basic Finner at Supersonic Speeds," NAVORD Report 4516, September 1960.
    • NAVORD Report
    • Shantz, I.1    Graves, R.T.2
  • 21
    • 13844276862 scopus 로고    scopus 로고
    • Application of System Identification to Aircraft at NASA Langley Research Center
    • January
    • Morelli, E. A. and Klein, V., "Application of System Identification to Aircraft at NASA Langley Research Center," Journal of Aircraft, 42(1):12-25, January 2005.
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    • Morelli, E.A.1    Klein, V.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.