Add to ORKGWind Tunnel Testing Of Generic Missile Model Has Been Carried $ Out To Generate Data For The Interference Factors Including The Panel-Panel Interference . Tests Have Been Carried Cut For Mach Numbers Of 0 .5, 0 .8, And 1 .2 . Three Fin Plan forms Giving A/Sm Of 0 .3, 0 .35 And 0 .4 (Aspect Ratios : 2 .0, 1 .4 And 0 .95) Have Been Selected For The Study
A research program was initiated for the purpose of investigating some of the problem areas in regar...
Results of the wind tunnel tests conducted on BAe R-80 model\ud are presented in this report. The ob...
Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 11-12).Mode of...
Wind Tunnel Testing Of Generic Missile Model Has Been Carried $ Out To Generate Data For The Interfe...
Wind tunnel tests were carried out to determine the aerodynamic characteristics of a 1/10th scale AG...
Tests were conducted in the Aerodynamic Wind Tunnel (4T) to evaluate the validity of weapon aerodyna...
This report presents the aerodynamic data generated on a 1/12 scale model of PRITHVI missile configu...
This Document Gives The Results Of Tests Conducted For The Armament Research And Development Establ...
Exploratory static-stability tests were made on models of the MK-84 weapon and a modular weapon conf...
Wind Tunnel Tests Were Carried Out To Determine The Aerodynamic Characteristics Of A 1/10th Scale Pa...
Wind tunnel tests were conducted to provide sting-support interference information for planning and ...
\ud In This Study A Method Is Presented For Estimating The Wingbvdy Interference Factor, K For Slend...
A parametric study of wrap-around-fin missile configurations has been conducted at Mach numbers from...
Results are presented of a free-flight investigation between Mach numbers of 0.7 to 1.3 and Reynolds...
Aerodynamic characteristics effected by parallel- staged simple aerodynamic configurations at Mach n...
A research program was initiated for the purpose of investigating some of the problem areas in regar...
Results of the wind tunnel tests conducted on BAe R-80 model\ud are presented in this report. The ob...
Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 11-12).Mode of...
Wind Tunnel Testing Of Generic Missile Model Has Been Carried $ Out To Generate Data For The Interfe...
Wind tunnel tests were carried out to determine the aerodynamic characteristics of a 1/10th scale AG...
Tests were conducted in the Aerodynamic Wind Tunnel (4T) to evaluate the validity of weapon aerodyna...
This report presents the aerodynamic data generated on a 1/12 scale model of PRITHVI missile configu...
This Document Gives The Results Of Tests Conducted For The Armament Research And Development Establ...
Exploratory static-stability tests were made on models of the MK-84 weapon and a modular weapon conf...
Wind Tunnel Tests Were Carried Out To Determine The Aerodynamic Characteristics Of A 1/10th Scale Pa...
Wind tunnel tests were conducted to provide sting-support interference information for planning and ...
\ud In This Study A Method Is Presented For Estimating The Wingbvdy Interference Factor, K For Slend...
A parametric study of wrap-around-fin missile configurations has been conducted at Mach numbers from...
Results are presented of a free-flight investigation between Mach numbers of 0.7 to 1.3 and Reynolds...
Aerodynamic characteristics effected by parallel- staged simple aerodynamic configurations at Mach n...
A research program was initiated for the purpose of investigating some of the problem areas in regar...
Results of the wind tunnel tests conducted on BAe R-80 model\ud are presented in this report. The ob...
Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 11-12).Mode of...