Static Aerodynamic Stability Characteristics Of A Body Of Revolution With Wraparound Fins At Mach Numbers From 0 5 To 1 3
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Static Aerodynamic Stability Characteristics Of A Body Of Revolution With Wraparound Fins At Mach Numbers From 0 5 To 1 3
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Author : John E. Vaughn
language : en
Publisher:
Release Date : 1972
Static Aerodynamic Stability Characteristics Of A Body Of Revolution With Wraparound Fins At Mach Numbers From 0 5 To 1 3 written by John E. Vaughn and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1972 with Guided missiles categories.
Experimental aerodynamic investigations were conducted in the AEDC-4T wind tunnel for several wraparound fins with straight and with swept leading edge mounted on bodies of revolution. Mach number ranged from 0.50 to 1.30 while angle of attack was varied from -6 degrees to 6 degrees at 0 degrees sideslip angle. Six component aerodynamic force and moment data were recorded on the complete missile configuration while simultaneously recording the aerodynamic normal force and bending moments acting on each fin. The results of these tests are presented in plotted form. (Author).
Some Effects Of Fin Plan Form On The Static Stability Of Fin Body Combinations At Mach Number 4 06
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Author : Edward F. Ulmann
language : en
Publisher:
Release Date : 1952
Some Effects Of Fin Plan Form On The Static Stability Of Fin Body Combinations At Mach Number 4 06 written by Edward F. Ulmann and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1952 with Aerodynamics, Supersonic categories.
Effects Of Body And Fin Deflections On The Aerodynamic Characteristics In Pitch Of A 0 065 Scale Model Of A Four Stage Rocket Configuration At Mach Numbers Of 1 41 And 1 82
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Author : Ross B. Robinson
language : en
Publisher:
Release Date : 1959
Effects Of Body And Fin Deflections On The Aerodynamic Characteristics In Pitch Of A 0 065 Scale Model Of A Four Stage Rocket Configuration At Mach Numbers Of 1 41 And 1 82 written by Ross B. Robinson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1959 with Mach number categories.
The Effect Of Cross Section Distribution On The Static Stability Characteristics Of Axi Symmetric Bodies At Mach Numbers Of 5 35 And 6 71
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Author : J. F. Reilly
language : en
Publisher:
Release Date : 1966
The Effect Of Cross Section Distribution On The Static Stability Characteristics Of Axi Symmetric Bodies At Mach Numbers Of 5 35 And 6 71 written by J. F. Reilly and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1966 with Aerodynamics, Hypersonic categories.
An investigation was made at hypersonic Mach numbers to determine the effects of cross-section distribution on the static stability characteristics of bodies of revolution and to obtain the aerodynamic characteristics of these bodies. All of the bodies tested had the same length and all were circular in cross-section. The bodies tested were conic, bi-conic, and tri-conic. The tests were performed at Mach numbers of 5.35 and 6.71, and at unit Reynolds numbers from 1.5 x 100,000 to 3.2 x 100,000 per centimeter. The results indicate that under certain test conditions a body with a forecone followed by a frustum or frustum-flare combination exhibits, through the flow mechanism on the upper quarter of the body, an adverse center of pressure travel in the low angle of attack region (0 to 5 degrees). For a given moment reference point this yields both stable and unstable trim-points. (Author).
Summary Of Static Stability And Drag Characteristics Of Axisymmetric Low Drag Shapes For The Subsonic To Hypersonic Mach Number Range
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Author : Amado A. Trujillo
language : en
Publisher:
Release Date : 1968
Summary Of Static Stability And Drag Characteristics Of Axisymmetric Low Drag Shapes For The Subsonic To Hypersonic Mach Number Range written by Amado A. Trujillo and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1968 with Drag (Aerodynamics) categories.
Static Stability Characteristics Of A Winged Body With Various Inlet Configurations At Mach Numbers Of 2 5 8 And 10
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Author : R. H. Burt
language : en
Publisher:
Release Date : 1964
Static Stability Characteristics Of A Winged Body With Various Inlet Configurations At Mach Numbers Of 2 5 8 And 10 written by R. H. Burt and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1964 with categories.
An experimental investigation has been conducted at Mach numbers of 2, 5, 8, and 10 to determine the static stability characteristics of a winged body configuration with various sizes and shapes of inlets attached. Selected results of the longitudinal stability and drag characteristics are presented for each configuration at the various mach numbers. The effect of inlet position along the model on the aerodynamic characteristics of two inlet configurations is presented for Mach numbers of 8 and 10. The investigation was performed at free-stream unit Reynolds numbers from 0.05 to 0.54 million per inch, angles of attack from -30 to 45 deg, and angles of yaw from 0 to 12 deg. (Author).
Static Aerodynamic Characteristics At Mach Numbers From 2 50 To 4 63 Of A Staged Airplane Model Designed For Cruise Above Mach 5
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Author :
language : en
Publisher:
Release Date : 1964
Static Aerodynamic Characteristics At Mach Numbers From 2 50 To 4 63 Of A Staged Airplane Model Designed For Cruise Above Mach 5 written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1964 with categories.
Static Stability Characteristics Of Blunt Low Fineness Ratio Bodies Of Revolution At A Mach Number Of 24 5 In Helium
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Author : Robert D. Witcofski
language : en
Publisher:
Release Date : 1964
Static Stability Characteristics Of Blunt Low Fineness Ratio Bodies Of Revolution At A Mach Number Of 24 5 In Helium written by Robert D. Witcofski and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1964 with Aerodynamics categories.
Aerodynamic Characteristics Of Two Bodies Of Revolution With Noses Of Varying Spherical Bluntness At Mach Numbers From 0 6 To 1 5
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Author : E. G Allee (Jr)
language : en
Publisher:
Release Date : 1973
Aerodynamic Characteristics Of Two Bodies Of Revolution With Noses Of Varying Spherical Bluntness At Mach Numbers From 0 6 To 1 5 written by E. G Allee (Jr) and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1973 with categories.
A wind tunnel investigation was conducted to determine the static stability characteristics of two bodies of revolution fitted with 2-, 3-, and 4-cal tangent ogive noses of varying spherical bluntness. Testing was conducted at Mach numbers from 0.6 to 1.5 and angles of attack from -2 to 14 deg. The major effect of blunting the noses was evidenced in the axial-force coefficient. Lengthening the noses from 2 to 4 cal caused a forward movement of the center-of-pressure location and a corresponding decrease in axial-force coefficient at Mach numbers of 1.0 and higher. Changing from a 5- to a 9-cal midbody resulted in an increase in axial-force coefficient and an aft movement of the center-of-pressure location. (Author).
Systematic Study Of The Static Stability Characteristics Of A Series Of Afterbody Flare Fin And Boattail Configurations At Mach Numbers From 1 57 To 2 87
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Author :
language : en
Publisher:
Release Date : 1959
Systematic Study Of The Static Stability Characteristics Of A Series Of Afterbody Flare Fin And Boattail Configurations At Mach Numbers From 1 57 To 2 87 written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1959 with categories.