Apparent Mass effects on parafoil dynamics

AIAA/AHS/ASEE Aerospace Design Conference, 1993

Volumn , Issue , 1993, Pages

  Lissaman, P B S ^a   Brown, Glen J ^b  

^a UNIVERSITY OF SOUTHERN CALIFORNIA   (United States)

^b Vertigo Inc   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

APPROXIMATE METHODS; FLIGHT VEHICLES; MASS EFFECTS; NOCV2; PARAFOILS; PARAMETRIC FORMS;

FLIGHT DYNAMICS;

EID: 84977771912     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (5)

1. Lamb, H., Hydrodynamics. Dover Publications, New York, 1945.
2. Bateman, H., “The Inertial Coefficients of an Airship in a Frictionless Fluid”, NACA Report 164, 1923.
3. Adkins, C.N., “The Added Mass and Inertia of Lightly Loaded Aircraft”, (Extensive analysis of the apparent mass of planar wings in potential flow, unpublished report), 1982.
4. Durand, W.F., Aerodynamic Theory. Durand Reprinting Committee, Caltech, 1943.
5. Etkin, B., Dynamics of Atmospheric Flight. Wiley, New York, 1972