Add to ORKGUnmanned Mars probe tested for drag, lift, static and dynamic stability at Mach number
Results obtained with two nose shapes tested at a Reynolds number per foot of 5 x 10(exp 6) at angle...
Effects of variations in launch vehicle nose configuration on steady and fluctuating pressures at tr...
Wind tunnel investigation of pressure distribution on blunted 15 deg half-cone wedge lifting-entry b...
Wind tunnel tests to determine flow patterns and pressure distributions around bluff afterbody in wa...
Transonic wind tunnel tests on Centaur and Able V models for steady and fluctuating pressure measur...
Pressure distribution studies in wind tunnel at Mach numbers 0.4 to 1.2 for protuberances and adjace...
Mach number and pressure measurements on afterbody of blunt-nose model in free flight at hypersonic ...
Overall fluctuating pressure levels of seven space shuttle launch configurations are presented. The ...
Pressure distributions over forward portion of project fire space-vehicle configuration at subsonic ...
Pressure distributions for blunt body wind tunnel models at supersonic speeds and angles of attack f...
Wind tunnel investigation of fluctuating pressures on Centaur model surface at transonic spee
Pressure distribution of spherically-blunted 60 deg half-angle cone in hypersonic flo
The investigations of pressure distributions are presented for aeroloads analysis at Mach numbers fr...
Base and afterbody pressures on boattailed bodies of revolution with hypersonic turbulent boundary l...
Unmanned Mars probe tested for drag, lift, static and dynamic stability at Mach number
Results obtained with two nose shapes tested at a Reynolds number per foot of 5 x 10(exp 6) at angle...
Effects of variations in launch vehicle nose configuration on steady and fluctuating pressures at tr...
Wind tunnel investigation of pressure distribution on blunted 15 deg half-cone wedge lifting-entry b...
Wind tunnel tests to determine flow patterns and pressure distributions around bluff afterbody in wa...
Transonic wind tunnel tests on Centaur and Able V models for steady and fluctuating pressure measur...
Pressure distribution studies in wind tunnel at Mach numbers 0.4 to 1.2 for protuberances and adjace...
Mach number and pressure measurements on afterbody of blunt-nose model in free flight at hypersonic ...
Overall fluctuating pressure levels of seven space shuttle launch configurations are presented. The ...
Pressure distributions over forward portion of project fire space-vehicle configuration at subsonic ...
Pressure distributions for blunt body wind tunnel models at supersonic speeds and angles of attack f...
Wind tunnel investigation of fluctuating pressures on Centaur model surface at transonic spee
Pressure distribution of spherically-blunted 60 deg half-angle cone in hypersonic flo
The investigations of pressure distributions are presented for aeroloads analysis at Mach numbers fr...
Base and afterbody pressures on boattailed bodies of revolution with hypersonic turbulent boundary l...
Unmanned Mars probe tested for drag, lift, static and dynamic stability at Mach number
Results obtained with two nose shapes tested at a Reynolds number per foot of 5 x 10(exp 6) at angle...
Effects of variations in launch vehicle nose configuration on steady and fluctuating pressures at tr...