From piston theory to a unified hypersonic-supersonic lifting surface method

Journal of Aircraft

Volumn 34, Issue 3, 1997, Pages 304-312

  Liu, D D ^a,c,d   Yao, Z X ^b,e   Sarhaddi, D ^b   Chavez, F ^b,f  

^a ARIZONA STATE UNIVERSITY   (United States)

^b ZONA TECHNOLOGY INC   (United States)

^c Mechanical and Aerospace Engineering   (United States)

^d AIAA   (United States)

^e IBM   (United States)

^f UNIVERSITY OF MARYLAND   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FLUTTER (AERODYNAMICS); HYPERSONIC AERODYNAMICS; LIFT; SUPERSONIC AERODYNAMICS; SYSTEM STABILITY;

ACKERET LIMIT; AERODYNAMIC INFLUENCE COEFFICIENT (AIC); LIFTING SURFACE METHOD; LINEAR LIFTING THEORY; MACH NUMBER; NEWTONIAN LIMIT;

WINGS;

EID: 0031140542     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.2199     Document Type: Article

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