Add to ORKGEffect of cross section shape on low speed aero- dynamic characteristics of low-wave drag hyper- sonic bod
An experimental investigation of the low-speed longitudinal, lateral, and directional stability char...
Effect of camber on aerodynamic characteristics of ogive-circular-cylindrical body at mach 2.0
Force, stability and control characteristics of three axisymmetric low fineness ratio reentry shapes...
Hypersonic aerodynamic performance of minimum wave drag bodies having various cross section
Stabilizer and tail assembly effects on overall aerodynamic characteristics of lifting bodies at hyp...
The drag of bodies has now assumed greater importance because, as shown in NACA RM L53I15a, 1953 and...
An experimental investigation was conducted to determine the effects of several variations in body s...
The drag of bodies has now assumed greater importance because, as shown in NACA RM L53I15a, 1953 and...
Transonic wind tunnel tests for aerodynamic characteristics of wing-body configuration
Optimum body length and volume design for minimal drag characteristics of hypersonic aircraf
An investigation has been made at Mach numbers from 1.50 to 4.63 to determine systematically the eff...
Effect of body cross sections and width-height ratio on performance of bodies and delta-wing- body c...
Longitudinal aerodynamic characteristics of hypersonic lifting body spacecraft with variable sweep w...
Hypersonic aerodynamic characteristics of low fineness ratio variable geometry logistics spacecraft ...
Drag characteristics of low drag bodies of revolution at Mach numbers from 0.6 to 4.
An experimental investigation of the low-speed longitudinal, lateral, and directional stability char...
Effect of camber on aerodynamic characteristics of ogive-circular-cylindrical body at mach 2.0
Force, stability and control characteristics of three axisymmetric low fineness ratio reentry shapes...
Hypersonic aerodynamic performance of minimum wave drag bodies having various cross section
Stabilizer and tail assembly effects on overall aerodynamic characteristics of lifting bodies at hyp...
The drag of bodies has now assumed greater importance because, as shown in NACA RM L53I15a, 1953 and...
An experimental investigation was conducted to determine the effects of several variations in body s...
The drag of bodies has now assumed greater importance because, as shown in NACA RM L53I15a, 1953 and...
Transonic wind tunnel tests for aerodynamic characteristics of wing-body configuration
Optimum body length and volume design for minimal drag characteristics of hypersonic aircraf
An investigation has been made at Mach numbers from 1.50 to 4.63 to determine systematically the eff...
Effect of body cross sections and width-height ratio on performance of bodies and delta-wing- body c...
Longitudinal aerodynamic characteristics of hypersonic lifting body spacecraft with variable sweep w...
Hypersonic aerodynamic characteristics of low fineness ratio variable geometry logistics spacecraft ...
Drag characteristics of low drag bodies of revolution at Mach numbers from 0.6 to 4.
An experimental investigation of the low-speed longitudinal, lateral, and directional stability char...
Effect of camber on aerodynamic characteristics of ogive-circular-cylindrical body at mach 2.0
Force, stability and control characteristics of three axisymmetric low fineness ratio reentry shapes...