메뉴 건너뛰기




Volumn 1, Issue , 2007, Pages 659-678

Aerodynamic analysis of body-strake configurations

Author keywords

[No Author keywords available]

Indexed keywords

DRAG COEFFICIENT; ESTIMATION; MACH NUMBER; MISSILES; TESTING;

EID: 35649014288     PISSN: 10485953     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2007-3939     Document Type: Conference Paper
Times cited : (4)

References (23)
  • 1
    • 85081479410 scopus 로고
    • Tourbillons de Corps Fusseles aux Incidence Eleve
    • l'Astronautique et l'Astronautique, June
    • Werle, H., "Tourbillons de Corps Fusseles aux Incidence Eleve," l'Astronautique et l'Astronautique, No 79, June 1979.
    • (1979) , Issue.79
    • Werle, H.1
  • 2
    • 35648991126 scopus 로고
    • A Wind Tunnel Investigation of Circular and Staked Cylinders in Transonic Cross Flow
    • 3318-76-01, Texas A&M Research Foundation, College Station, TX, Nov
    • Macha, J. M., "A Wind Tunnel Investigation of Circular and Staked Cylinders in Transonic Cross Flow," TAMU Rep. 3318-76-01, Texas A&M Research Foundation, College Station, TX, Nov. 1976.
    • (1976) TAMU Rep
    • Macha, J.M.1
  • 3
    • 85003283005 scopus 로고    scopus 로고
    • Macha, J. M., Drag of Circular Cylinders at Transonic Mach Numbers, JA, 14, No. 6, June 1977, pp. 605-607.
    • Macha, J. M., "Drag of Circular Cylinders at Transonic Mach Numbers," JA, Vol. 14, No. 6, June 1977, pp. 605-607.
  • 5
    • 3843106885 scopus 로고
    • Prediction of Static Aerodynamic Characteristics for Slender Bodies Alone and With Lifting Surfaces to Very High Angles of Attack
    • Sep
    • Jorgensen, L. H., "Prediction of Static Aerodynamic Characteristics for Slender Bodies Alone and With Lifting Surfaces to Very High Angles of Attack," NASA TR R-474, Sep. 1977.
    • (1977) NASA TR , vol.R-474
    • Jorgensen, L.H.1
  • 7
    • 0006906833 scopus 로고    scopus 로고
    • Drag of Cylinders of Simple Shapes
    • 619, Oct. 1937
    • Lindsey, W. F., "Drag of Cylinders of Simple Shapes," NACA Rep. 619, Oct. 1937.
    • NACA Rep
    • Lindsey, W.F.1
  • 8
    • 85081476122 scopus 로고
    • The Drag of Finite-Length Cylinders Determined from Flight Tests at High Reynolds Numbers for a Mach Number Range from 0.4 to 1.3
    • Welsh, C. J., "The Drag of Finite-Length Cylinders Determined from Flight Tests at High Reynolds Numbers for a Mach Number Range from 0.4 to 1.3," NACA TN 2941, 1952.
    • (1952) NACA TN , vol.2941
    • Welsh, C.J.1
  • 9
    • 4243772104 scopus 로고
    • Experimental Aerodynamic Characteristics for a Cylindrical Body of Revolution With Various Noses at Angles of Attack from 0° to 58° and Mach Numbers from 0.6 to 2.0
    • Dec
    • Jorgensen, L. H., and Nelson, E. R., "Experimental Aerodynamic Characteristics for a Cylindrical Body of Revolution With Various Noses at Angles of Attack from 0° to 58° and Mach Numbers from 0.6 to 2.0," NASA TM X-3128, Dec. 1974.
    • (1974) NASA TM , vol.X-3128
    • Jorgensen, L.H.1    Nelson, E.R.2
  • 10
    • 85003249943 scopus 로고
    • Wind-Tunnel Force and Flow Visualization Data at Mach Numbers From 1.6 to 4.63 for a Series of Bodies of Revolution at Angles of Attack From -4° to 60°
    • 78813
    • Landrum, E. J., and Babb, C. D., "Wind-Tunnel Force and Flow Visualization Data at Mach Numbers From 1.6 to 4.63 for a Series of Bodies of Revolution at Angles of Attack From -4° to 60°," NASA TM 78813, 1979.
    • (1979) NASA TM
    • Landrum, E.J.1    Babb, C.D.2
  • 11
    • 85081487471 scopus 로고
    • Normal Force, Pitching Moment and Side Force of Forbody-Cylinder Combinations for Angles of Attack Up to 90 Degrees and Mach Numbers Up to 5
    • London, UK, Anon
    • Anon., "Normal Force, Pitching Moment and Side Force of Forbody-Cylinder Combinations for Angles of Attack Up to 90 Degrees and Mach Numbers Up to 5," ESDU International Item 89014, London, UK, 1989.
    • (1989) ESDU International Item , pp. 89014
  • 12
    • 85081476249 scopus 로고    scopus 로고
    • Winter, H., Flow Phenomena on Plates and Airfoils of Short Span, NACA TM 798, 1936. The data is available in Stahal, W. H., Aerodynamics of Low Aspect Ratio Wings, Article Xs 3, AGARD LS 98, 1998.
    • Winter, H., "Flow Phenomena on Plates and Airfoils of Short Span," NACA TM 798, 1936. The data is available in Stahal, W. H., "Aerodynamics of Low Aspect Ratio Wings,", Article Xs 3, AGARD LS 98, 1998.
  • 13
    • 85081490609 scopus 로고
    • Effect of Cross-Section Shape on the Aero Characteristics at Mach Numbers to 4.63
    • NASA TN-D-1620, Mar
    • Fuller, D. E., Shaw, D. S., and Wassum, D. L., "Effect of Cross-Section Shape on the Aero Characteristics at Mach Numbers to 4.63," NASA TN-D-1620, Mar. 1983.
    • (1983)
    • Fuller, D.E.1    Shaw, D.S.2    Wassum, D.L.3
  • 14
    • 85081475236 scopus 로고    scopus 로고
    • Hoak, D. E., (Project Engineer) and Ellison, D. E., (Chief Scientist) USAF Stability and Control Dactom, Flight Control Division, AF Flight Dynamics laboratory, (now AFRL) Wright-Patterson AF Base, OH, 1968.
    • Hoak, D. E., (Project Engineer) and Ellison, D. E., (Chief Scientist) "USAF Stability and Control Dactom," Flight Control Division, AF Flight Dynamics laboratory, (now AFRL) Wright-Patterson AF Base, OH, 1968.
  • 15
    • 85081492425 scopus 로고    scopus 로고
    • Hemsch, M. J., Component Build-Up Method for Engineering Analysis of Missiles at Low-to-High Angles of Attack. Chapter 4 in Tactical Missiles Aerodynamics: Prediction Methods, Progress in Astronautics and Aeronautics, 142, AIAA Publication, 1992.
    • Hemsch, M. J., "Component Build-Up Method for Engineering Analysis of Missiles at Low-to-High Angles of Attack." Chapter 4 in "Tactical Missiles Aerodynamics: Prediction Methods," Progress in Astronautics and Aeronautics, Vol. 142, AIAA Publication, 1992.
  • 16
    • 0003817459 scopus 로고    scopus 로고
    • USAF Research Laboratory, Report AFRL-VAWP-TR-1988-3009, Wright-Patterson AFB, OH, Feb
    • Blake, W. B., "Missile Datcom User's Manual - 1997 Fortran 90 Version," USAF Research Laboratory, Report AFRL-VAWP-TR-1988-3009, Wright-Patterson AFB, OH, Feb. 1998.
    • (1998) Missile Datcom User's Manual - 1997 Fortran 90 Version
    • Blake, W.B.1
  • 17
    • 85081475948 scopus 로고
    • Static Stability Characteristics of a Series of Hypersonic Boost-Glide Configurations at Mach Numbers 1.41 and 2.01
    • Aug
    • Foster, G. V., "Static Stability Characteristics of a Series of Hypersonic Boost-Glide Configurations at Mach Numbers 1.41 and 2.01," NASA TM X-167, Aug. 1957.
    • (1957) NASA TM , vol.X-167
    • Foster, G.V.1
  • 20
    • 4243772104 scopus 로고
    • Experimental Aerodynamic Characteristics for a Cylindrical Body of Revolution With Side Strakes and Various Noses at Angles of Attack from 0° to 58° and Mach Numbers from 0.6 to 2.0
    • March
    • Jorgensen, L. H., "Experimental Aerodynamic Characteristics for a Cylindrical Body of Revolution With Side Strakes and Various Noses at Angles of Attack from 0° to 58° and Mach Numbers from 0.6 to 2.0," NASA TM X-3130, March 1975.
    • (1975) NASA TM , vol.X-3130
    • Jorgensen, L.H.1
  • 22
    • 18144399656 scopus 로고
    • Wind-Tunnel Investigation at a Mach Number of 2.01 of the Aerodynamic Characteristics in Combined Angle of Attack and Sideslip of Several Hypersonic Missile Configurations With Various Canard Controls
    • March
    • Robinson, R. B., "Wind-Tunnel Investigation at a Mach Number of 2.01 of the Aerodynamic Characteristics in Combined Angle of Attack and Sideslip of Several Hypersonic Missile Configurations With Various Canard Controls," NACA RM L58A21, March 1958.
    • (1958) NACA RM L58A21
    • Robinson, R.B.1
  • 23
    • 85081482213 scopus 로고
    • Longitudinal Stability and Control Characteristics at Mach Numbers of 2.01, 4.65, and 6.8 of Two Hypersonic Missile Configurations
    • Sep
    • Spearman M. L., and Robinson, R. B., "Longitudinal Stability and Control Characteristics at Mach Numbers of 2.01, 4.65, and 6.8 of Two Hypersonic Missile Configurations," NASA TM X-46, Sep. 1959.
    • (1959) NASA TM , vol.X-46
    • Spearman, M.L.1    Robinson, R.B.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.