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Suggested Topics within your search.
Suggested Topics within your search.
- Noses (Space vehicles)
- Space vehicles 4
- Testing 4
- Aerodynamics 3
- Aerodynamics, Hypersonic 3
- Atmospheric entry 3
- Aerodynamic heating 2
- Angle of attack (Aerodynamics) 2
- Data processing 2
- Design and construction 2
- Reynolds number 2
- Shock waves 2
- Aerodynamic load 1
- Aerodynamics, Supersonic 1
- Ballistic missiles 1
- Cone 1
- Heat 1
- Mach number 1
- Measurement 1
- Microwave antennas 1
- Plasma sheaths 1
- Pressure 1
- Radiation and absorption 1
- Reusable space vehicles 1
- Saturn launch vehicles 1
- Shielding (Heat) 1
- Sphere 1
- Staging (Space flight) 1
- Supersonic wind tunnels 1
- Thermal conductivity 1
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1
Turbulent boundary-layer separation induced by flares on cylinders at zero angle of attack /
Published 1961Government Document Book
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2
Effect of unit Reynolds number, nose bluntness, angle of attack, and roughness on transition on a 5° half-angle cone at Mach 8 /
Published 1969Online Access
Government Document eBook -
3
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4
Experimental base pressures on 9 ̊spherically blunted cones at Mach numbers from 10.5 to 20 /
Published 1968Online Access
Government Document eBook -
5
The useful heat capacity of several materials for ballistic nose-cone construction /
Published 1957Government Document Book -
6
Free-flight test of a technique for inflating an NASA 12-foot-diameter sphere at high altitudes /
Published 1959Government Document Book -
7
A coupled computer code for the transient thermal response and ablation of non-charring heat shields and nose tips /
Published 1970Government Document Book -
8
Performance of a microwave antenna system in the shoulder region of a blunt reentry nose cone /
Published 1973Government Document Book -
9
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10
A method for determining surface pressures on blunt bodies of revolution at small angles of attack in supersonic flow /
Published 1968Online Access
Government Document eBook -
11
Flight-test analysis of Apollo heat-shield material using the pacemaker vehicle system /
Published 1968Online Access
Government Document eBook -
12
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13
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14
Measured and predicted shock shapes and aerodynamic coefficients for blunted cones at incidence in air at Mach 5.9 /
Published 1980Government Document Book -
15
Synthesis of optimum structural designs for conical and tension shell Mars entry capsules /
Published 1969Search for the full-text version of this title in HathiTrust
Government Document Book