Author: James O. Nichols
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 132
Book Description
This summary document was prepared in order to facilitate dissemination of a large amount of missile aerodynamic data which has recently been declassified. Only summary data are presented in this report, but a list of reference documents provides sources of detailed data. Most of the configurations considered are suitable for highly maneuverable air-to-air or surface to air missiles; however, data for a few air-to-surface, cruise missile, and one projectile configuration are also presented. The Mach number range of the data is from about 0.2 to 4.63; however, data for most configurations cover only a portion of this range. The following aerodynamic characteristics at various Mach numbers and zero angle of attack are presented.
Analysis and Compilation of Missile Aerodynamic Data: Data presentation and analysis
Author: James O. Nichols
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 132
Book Description
This summary document was prepared in order to facilitate dissemination of a large amount of missile aerodynamic data which has recently been declassified. Only summary data are presented in this report, but a list of reference documents provides sources of detailed data. Most of the configurations considered are suitable for highly maneuverable air-to-air or surface to air missiles; however, data for a few air-to-surface, cruise missile, and one projectile configuration are also presented. The Mach number range of the data is from about 0.2 to 4.63; however, data for most configurations cover only a portion of this range. The following aerodynamic characteristics at various Mach numbers and zero angle of attack are presented.
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 132
Book Description
This summary document was prepared in order to facilitate dissemination of a large amount of missile aerodynamic data which has recently been declassified. Only summary data are presented in this report, but a list of reference documents provides sources of detailed data. Most of the configurations considered are suitable for highly maneuverable air-to-air or surface to air missiles; however, data for a few air-to-surface, cruise missile, and one projectile configuration are also presented. The Mach number range of the data is from about 0.2 to 4.63; however, data for most configurations cover only a portion of this range. The following aerodynamic characteristics at various Mach numbers and zero angle of attack are presented.
Analysis and Compilation of Missile Aerodynamic Data. Volume 1: Data Presentation and Analysis
Author: James O. Nichols
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 132
Book Description
This summary document was prepared in order to facilitate dissemination of a large amount of missile aerodynamic data which has recently been declassified. Only summary data are presented in this report, but a list of reference documents provides sources of detailed data. Most of the configurations considered are suitable for highly maneuverable air-to-air or surface to air missiles; however, data for a few air-to-surface, cruise missile, and one projectile configuration are also presented. The Mach number range of the data is from about 0.2 to 4.63; however, data for most configurations cover only a portion of this range. The following aerodynamic characteristics at various Mach numbers and zero angle of attack are presented.
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 132
Book Description
This summary document was prepared in order to facilitate dissemination of a large amount of missile aerodynamic data which has recently been declassified. Only summary data are presented in this report, but a list of reference documents provides sources of detailed data. Most of the configurations considered are suitable for highly maneuverable air-to-air or surface to air missiles; however, data for a few air-to-surface, cruise missile, and one projectile configuration are also presented. The Mach number range of the data is from about 0.2 to 4.63; however, data for most configurations cover only a portion of this range. The following aerodynamic characteristics at various Mach numbers and zero angle of attack are presented.
Analysis and Compilation of Missile Aerodynamic Data
Author: James O. Nichols
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages :
Book Description
This summary document was prepared in order to facilitate dissemination of a large amount of missile aerodynamic data which has recently been declassified. Only summary data are presented in this report, but a list of reference documents provides sources of detailed data. Most of the configurations considered are suitable for highly maneuverable air-to-air or surface to air missiles; however, data for a few air-to-surface, cruise missile, and one projectile configuration are also presented. The Mach number range of the data is from about 0.2 to 4.63; however, data for most configurations cover only a portion of this range. The following aerodynamic characteristics at various Mach numbers and zero angle of attack are presented.
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages :
Book Description
This summary document was prepared in order to facilitate dissemination of a large amount of missile aerodynamic data which has recently been declassified. Only summary data are presented in this report, but a list of reference documents provides sources of detailed data. Most of the configurations considered are suitable for highly maneuverable air-to-air or surface to air missiles; however, data for a few air-to-surface, cruise missile, and one projectile configuration are also presented. The Mach number range of the data is from about 0.2 to 4.63; however, data for most configurations cover only a portion of this range. The following aerodynamic characteristics at various Mach numbers and zero angle of attack are presented.
Analysis and Compilation of Missile Aerodynamic Data: Data presentation and analysis
Author: James O. Nichols
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 132
Book Description
This summary document was prepared in order to facilitate dissemination of a large amount of missile aerodynamic data which has recently been declassified. Only summary data are presented in this report, but a list of reference documents provides sources of detailed data. Most of the configurations considered are suitable for highly maneuverable air-to-air or surface to air missiles; however, data for a few air-to-surface, cruise missile, and one projectile configuration are also presented. The Mach number range of the data is from about 0.2 to 4.63; however, data for most configurations cover only a portion of this range. The following aerodynamic characteristics at various Mach numbers and zero angle of attack are presented.
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 132
Book Description
This summary document was prepared in order to facilitate dissemination of a large amount of missile aerodynamic data which has recently been declassified. Only summary data are presented in this report, but a list of reference documents provides sources of detailed data. Most of the configurations considered are suitable for highly maneuverable air-to-air or surface to air missiles; however, data for a few air-to-surface, cruise missile, and one projectile configuration are also presented. The Mach number range of the data is from about 0.2 to 4.63; however, data for most configurations cover only a portion of this range. The following aerodynamic characteristics at various Mach numbers and zero angle of attack are presented.
Analysis and Compilation of Missile Aerodynamic Data
Author: John E. Burkhalter
Publisher:
ISBN:
Category : Guided missiles
Languages : en
Pages : 0
Book Description
Publisher:
ISBN:
Category : Guided missiles
Languages : en
Pages : 0
Book Description
Analysis and Compilation of Missile Aerodynamic Data
Analysis and Compilation of Missile Aerodynamic Data. Volume 2: Performance Analysis
Analysis and Compilation of Missile Aerodynamic Data
Author: John E. Burkhalter
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 310
Book Description
This report provides a general analysis of the flight dynamics of several surface-to-air and two air-to-air missile configurations. The analysis involves three phases: vertical climb, straight and level flight, and constant altitude turn. Wind tunnel aerodynamic data and full scale missile characteristics are used when available; unkonwn data are estimated. For the constant altitude turn phase, a three degree of freedom flight simulation is used. Important parameters considered in this analysis are the vehicle weight, Mach number, heading angle, thrust level, sideslip angle, g loading, and time to make the turn. The actual flight path during the turn is also determined. Results are presented in graphical form.
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 310
Book Description
This report provides a general analysis of the flight dynamics of several surface-to-air and two air-to-air missile configurations. The analysis involves three phases: vertical climb, straight and level flight, and constant altitude turn. Wind tunnel aerodynamic data and full scale missile characteristics are used when available; unkonwn data are estimated. For the constant altitude turn phase, a three degree of freedom flight simulation is used. Important parameters considered in this analysis are the vehicle weight, Mach number, heading angle, thrust level, sideslip angle, g loading, and time to make the turn. The actual flight path during the turn is also determined. Results are presented in graphical form.
Interim Report on Analysis and Compilation of Missile Aerodynamic Data
Author: James O. Nichols
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 84
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 84
Book Description