Doris Cohen

Doris Cohen bụ onye ọka mmụta mgbakọ na mwepụ nke Amerika na narị afọ nke iri abụọ na onye na-ahụ maka ikuku. Ọ rụrụ ọrụ na Langley Memorial Aeronautical Laboratory nke National Advisory Committee for Aeronautics (NACA, onye bu NASA ụzọ). N'afọ 1941, akụkọ nyocha o bipụtara mere ka ọ bụrụ nwanyị edemede mbụ nke NACA.

Ọ lụrụ, ma soro ya bu, aerodynamicist R. T. Jones. Ya na ya guzobere Vega Instrument Co., ụlọ ọrụ na-emepụta onyokomita, n'afọ 1957. 

 Akwụkwọ akụkọ 

 Nnyocha nke nkwụsi ike nke ụgbọelu na Free Controls na Robert T. Jones (1941) 
 A Graphical Method of Determining Pressure Distribution in Two-dimensional Flow na Robert T. Jones (1941) 
 Nkọwa nke Ibu n'elu nku na-ehicha n'azụ (1942) 
 Ụzọ iji chọpụta camber na twist nke elu iji kwado nkesa e nyere nke lift (1942) 
 Nkọwapụta nke ụdị atụmatụ kachasị mma maka ebe nchịkwa na Robert T. Jones (1942) 
 Nnyocha Theoretical nke Rolling Oscillations nke ụgbọelu na Ailerons Free (1944) 
 Nnyocha nyocha nke nkwụsi ike nke F8F Dropping Model na nkwụsi elu na-akpaghị aka (1945) 
 Ụzọ iji chọpụta camber na twist nke elu iji kwado nkesa e nyere nke lift, yana itinye n'ọrụ na ibu n'elu nku azụ (1945) 
 The Theoretical Lift of Flat Swept-back Wings at Supersonic Speeds (1948) 
 Theoretical Loading at Supersonic Speeds of Flat Swept-back Wings with Interacting Trailing and Leading Edges (1949) 
 Usoro na chaatị maka Supersonic Lift na Drag nke Flat Swept-back Wings na Interacting Leading na Trailing Edges (1950) 
 Usoro maka Loading Supersonic, Lift, na Drag nke Flat Swept-Back Wings na Leading Edges Behind the Mach Line (1951) 
 Nnyocha echiche nke Supersonic Lift na Drag of Thin, Sweptback Wings na Increased Sweep nso Root na Morris D. Friedman (1953) 
 Nhazi nke Fusiform Bodies iji belata Wave Drag na Supersonic Speeds na Morris D Friedman (1954) 

 Edemsibịa 

 Njikọ mpụga 

 Ndepụta maka ọrụ Cohen na NASA
Otú:Mmadụ ndi di ndụ