Wind-tunnel Tests of Single- and Dual-rotating Tractor Propellers of Large Blade Width
Wind-tunnel Tests of Single- and Dual-rotating Pusher Propellers Having from Three to Eight Blades
Wind-tunnel Tests of Four Curtiss Propellers Embodying Different Blade Sections
Wind-tunnel Tests of Eight-blade Single and Dual-rotating Propellers in the Tractor Position
Wind-tunnel Tests of a Dual-rotating Propeller Having One Component Locked or Windmilling
Wind-tunnel Investigation of Ailerons on a Low-drag Airfoil III : the Effect of Tabs
The reaction jet as a means of propulsion at high speeds
Theory of the inlet and exhaust processes of internal-combustion engines
The influence of blade-width distribution on propeller characteristics
The efficiency of electrical discharges for electric propulsion
The Effect of Pitch on Force and Moment Characteristics of Full-scale Propellers of Five Solidities
The application of modular concepts for electric propulsion power conditioning.
Study of magnetic annular plasma accelerator Summary report, 15 Apr. 1964 - 14 Jan. 1966
Studies of nozzle ablative material performance for large solid boosters Final report
Static Characteristics of Curtiss Propellers Having Different Blade Sections
Rainbow: A New Ultra-High Efficiency Solar Array
Proposed Flight Research of a Dual-Bell Rocket Nozzle Using the NASA F-15 Airplane
Propeller selection from aerodynamic considerations
Propeller Flight Investigation to Determine the Effects of Blade Loading
Promises and potentialities of electric propulsion status of thrustor performance.
Promises and potentialities of electric propulsion - Status of thrustor performance.
Performance of high-efficiency advanced triple-junction solar panels for the LILT Mission Dawn
OPERATIONAL TECHNIQUE FOR TRANSITION OF SEVERAL TYPES OF V STOL AIRCRAFT
Nearfield Unsteady Pressures at Cruise Mach Numbers for a Model Scale Counter-Rotation Open Rotor
Mid-frequency comparison FEA/BEA and SEA spacecraft predictions
Method of calculating performance of dual-rotating propellers from airfoil characteristics
Maximum velocity of a rocket /1935/
M-1 injector development - Philosophy and implementation