Add to ORKGExperimentally determined local flow properties and drag coefficients for family of blunt bodies at Mach numbers from 2.49 to 4.6
Pressure distributions and drag coefficients of 18 constant length and volume slender bodies of revo...
An investigation of anomalies observed in wind tunnel force tests of a blunt body configuration was ...
An experimental investigation in the Langley Gas Dynamics Laboratory has been made of the flow separ...
Pressure distributions for blunt body wind tunnel models at supersonic speeds and angles of attack f...
Transonic wind tunnel study of aerodynamic characteristics of blunt reentry vehicles at varying angl...
NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in...
Pressure distributions, aerodynamic coefficients, and shock shapes were measured on blunt bodies of ...
Mach number and pressure measurements on afterbody of blunt-nose model in free flight at hypersonic ...
Results of tests to determine the aerodynamic forces and moments on bodies of revolution at angles o...
Pressure distributions and forces for a series of four bodies of revolution having nose-fineness rat...
Measurements of the local heat transfer and pressure distribution have been made on six 2-inch-diame...
Pressure distributions and shock shapes for a series of cylindrical afterbodies having nose fineness...
"October 1967 ."Includes bibliographical references.Mode of access: Internet.Mode of access: World W...
Effect of nose bluntness, fineness ratio, cone angle, and model base on aerodynamic characteristics ...
Experimental drag measurements at zero angle of attack for various theoretical minimum drag nose sha...
Pressure distributions and drag coefficients of 18 constant length and volume slender bodies of revo...
An investigation of anomalies observed in wind tunnel force tests of a blunt body configuration was ...
An experimental investigation in the Langley Gas Dynamics Laboratory has been made of the flow separ...
Pressure distributions for blunt body wind tunnel models at supersonic speeds and angles of attack f...
Transonic wind tunnel study of aerodynamic characteristics of blunt reentry vehicles at varying angl...
NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in...
Pressure distributions, aerodynamic coefficients, and shock shapes were measured on blunt bodies of ...
Mach number and pressure measurements on afterbody of blunt-nose model in free flight at hypersonic ...
Results of tests to determine the aerodynamic forces and moments on bodies of revolution at angles o...
Pressure distributions and forces for a series of four bodies of revolution having nose-fineness rat...
Measurements of the local heat transfer and pressure distribution have been made on six 2-inch-diame...
Pressure distributions and shock shapes for a series of cylindrical afterbodies having nose fineness...
"October 1967 ."Includes bibliographical references.Mode of access: Internet.Mode of access: World W...
Effect of nose bluntness, fineness ratio, cone angle, and model base on aerodynamic characteristics ...
Experimental drag measurements at zero angle of attack for various theoretical minimum drag nose sha...
Pressure distributions and drag coefficients of 18 constant length and volume slender bodies of revo...
An investigation of anomalies observed in wind tunnel force tests of a blunt body configuration was ...
An experimental investigation in the Langley Gas Dynamics Laboratory has been made of the flow separ...