Add to ORKGA Systematic Study Has Been Undertaken To Investigate The Effects Of Flare On An Axisymmetric Body, Typical Of Missile Configurations . Measurements Have Been Made Of The Longitudinal Aerodynamic Characteristics Of The Model For Angles Of Attack Upto 20 Deg . And Mach Numbers Ranging From 0.5 To 3.0. Flares Of Angles 5° , 10 ° , 15° And 20° At Three Axial Positions Have Been Considered In The Study. Test Results Have Been Presented In The Form Of Tables And Aerodynamic Characteristic Plots For Typical Subsonic, Transonic And Supersonic Mach Numbers Are Included .\u
An investigation of the aerodynamic characteristics of several hypersonic missile configurations wit...
Experimental aerodynamic characteristics of a low-drag missile concept with a body of circular cross...
Results are presented of a free-flight investigation between Mach numbers of 0.7 to 1.3 and Reynolds...
This proposal describes the first phase of the work comtemplated for the Missile Design Manual . The...
An experimental study has been performed to develop a large force and moment aerodynamic data set on...
A study has been made of the experimental and theoretical aerodynamic characteristics for some gener...
An experimental study has been performed at M∞=8.2 and Re∞/cm=93000 to examine: 1. The effect of st...
A study of the aerodynamic characteristics of two missile configurations has been performed using th...
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 magnitude and the effects of boundary-layer separation on normal-force-curve slopes, centers of ...
Transonic static aerodynamic characteristics of blunt cone cylinder body with flared afterbodies of ...
The problem of predicting the induced roll phenomena associated with finned missiles at high angles ...
The article of record as published may be found at https://doi.org/10.2514/3.26260Wind-tunnel tests ...
uNgN;;:;-a;,Y& By autho~ti and drag characte&tics of a missile c configuration having a body...
An investigation of the aerodynamic characteristics of several hypersonic missile configurations wit...
Experimental aerodynamic characteristics of a low-drag missile concept with a body of circular cross...
Results are presented of a free-flight investigation between Mach numbers of 0.7 to 1.3 and Reynolds...
This proposal describes the first phase of the work comtemplated for the Missile Design Manual . The...
An experimental study has been performed to develop a large force and moment aerodynamic data set on...
A study has been made of the experimental and theoretical aerodynamic characteristics for some gener...
An experimental study has been performed at M∞=8.2 and Re∞/cm=93000 to examine: 1. The effect of st...
A study of the aerodynamic characteristics of two missile configurations has been performed using th...
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 magnitude and the effects of boundary-layer separation on normal-force-curve slopes, centers of ...
Transonic static aerodynamic characteristics of blunt cone cylinder body with flared afterbodies of ...
The problem of predicting the induced roll phenomena associated with finned missiles at high angles ...
The article of record as published may be found at https://doi.org/10.2514/3.26260Wind-tunnel tests ...
uNgN;;:;-a;,Y& By autho~ti and drag characte&tics of a missile c configuration having a body...
An investigation of the aerodynamic characteristics of several hypersonic missile configurations wit...
Experimental aerodynamic characteristics of a low-drag missile concept with a body of circular cross...
Results are presented of a free-flight investigation between Mach numbers of 0.7 to 1.3 and Reynolds...