Author: James O. Nichols
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 326
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 : 326
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 : 326
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: 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.
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 : 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: 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.
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