Ground testing facility for modeling real projectile flight heating in earth atmosphere

Journal of Thermophysics and Heat Transfer

Volumn 16, Issue 1, 2002, Pages 101-108

  Seiler, Friedrich ^a   Werner, Udo ^a   Patz, Gunther ^a  

^a FRENCH GERMAN RESEARCH INSTITUTE OF SAINT LOUIS   (France)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC HEATING; BALLISTICS; BOUNDARY CONDITIONS; BOUNDARY LAYERS; COMPRESSED AIR; FLIGHT DYNAMICS; HEAT FLUX; HIGH PRESSURE EFFECTS; INFRARED RADIATION; MATHEMATICAL MODELS; MATHEMATICAL TRANSFORMATIONS; NOSE CONES; PROJECTILES; REYNOLDS NUMBER; TEST FACILITIES; TURBULENT FLOW;

AEROTHERMOBALLISTICS; HYPERSONIC PROJECTILES;

HYPERSONIC AERODYNAMICS;

AIR TEMPERATURE; ANALYTICAL METHOD; BOUNDARY LAYER; GROUND-BASED MEASUREMENT; SURFACE TEMPERATURE; TURBULENT FLOW;

EID: 0036098026     PISSN: 08878722     EISSN: 15336808     Source Type: Journal    
DOI: 10.2514/2.6657     Document Type: Article

References (8)

1. Prediction of surface heating of a projectile flying in RAMAC 30 of ISL
2. Die laminare grenzschicht bei einem mit überschallgeschwindigkeit angestrrömten nichtangestellten kreiskegel
3. Hypersonic, turbulent skin-friction and heat-transfer measurements on a sharp cone
4. Theoretische und experimentelle untersuchung der turbulenten grenzschicht hinter einem kolben im stoßrohr
5. Theoretical and experimental investigation of bow wave heating at the conical nose of projectiles
6. Aerothermal study of a projectile in flight: Experiment-computation comparison