The problem of predicting the induced roll phenomena associated with finned missiles at high angles of attack has been approached by examining the interaction between the body wake vortex system and the finned surfaces of the missile. The application of the classic Blasius moment integral to this problem permits the independent evaluation of each singularity in the flow field which may contribute to the moments. This method is applicable to missiles employing fin schemes of any geometry and is used herein to analyze the induced roll of a typical cruciform missile configuration. A computer program has been developed to generate numerical solutions utilizing those parameters which affect the magnitude and direction of the induced roll. (Autho...
The method for predicting wing- tail interference whereby the trailing vortex system behind lifting ...
A Systematic Study Has Been Undertaken To Investigate The Effects Of Flare On An Axisymmetric Body, ...
This paper provides a brief overview of the activities undertaken by the Missile Facet of NATO STO A...
Previous analytical studies endeavoring to account for vortex induced rolling moments on missiles ha...
A method is presented for estimating the rolling moments caused by wing-tail interference for missil...
This proposal describes the first phase of the work comtemplated for the Missile Design Manual . The...
This Technical Report Covers The Work Carried Out Under A Memorandum Of Understanding Between NAL An...
This Technical Report Covers The Work Carried Out Under A Memorandum Of Understanding Between NAL An...
The article of record as published may be found at https://doi.org/10.2514/3.26260Wind-tunnel tests ...
An experimental study has been performed to develop a large force and moment aerodynamic data set on...
Hybrid Reynolds Average Navier-Stokes (RANS) - Large Eddy Simulations (LES) have been applied to pre...
An experimental and theoretical investigation of the longitudinal and lateral-directional stability ...
AbstractThe modern high performance air vehicles are required to have extreme maneuverability, which...
The lift, pitching-moment, and drag characteristics of a missile configuration having a body of fine...
uNgN;;:;-a;,Y& By autho~ti and drag characte&tics of a missile c configuration having a body...
The method for predicting wing- tail interference whereby the trailing vortex system behind lifting ...
A Systematic Study Has Been Undertaken To Investigate The Effects Of Flare On An Axisymmetric Body, ...
This paper provides a brief overview of the activities undertaken by the Missile Facet of NATO STO A...
Previous analytical studies endeavoring to account for vortex induced rolling moments on missiles ha...
A method is presented for estimating the rolling moments caused by wing-tail interference for missil...
This proposal describes the first phase of the work comtemplated for the Missile Design Manual . The...
This Technical Report Covers The Work Carried Out Under A Memorandum Of Understanding Between NAL An...
This Technical Report Covers The Work Carried Out Under A Memorandum Of Understanding Between NAL An...
The article of record as published may be found at https://doi.org/10.2514/3.26260Wind-tunnel tests ...
An experimental study has been performed to develop a large force and moment aerodynamic data set on...
Hybrid Reynolds Average Navier-Stokes (RANS) - Large Eddy Simulations (LES) have been applied to pre...
An experimental and theoretical investigation of the longitudinal and lateral-directional stability ...
AbstractThe modern high performance air vehicles are required to have extreme maneuverability, which...
The lift, pitching-moment, and drag characteristics of a missile configuration having a body of fine...
uNgN;;:;-a;,Y& By autho~ti and drag characte&tics of a missile c configuration having a body...
The method for predicting wing- tail interference whereby the trailing vortex system behind lifting ...
A Systematic Study Has Been Undertaken To Investigate The Effects Of Flare On An Axisymmetric Body, ...
This paper provides a brief overview of the activities undertaken by the Missile Facet of NATO STO A...