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Mertsheimer's variable exhaust nozzle
Carbureter Design for the C. F. R. Detonation Engine
A PROCEDURE FOR DETERMINING DIESEL NOZZLE SPRAY CHARACTERISTICS
Design of nozzles for the individual cylinder exhaust jet propulsion system
A NEW FUEL INJECTION NOZZLE FOR HIGH SPEED DIESEL AND GASOLINE INJECTION ENGINES
Principles and methods of rating and testing centrifugal superchargers
An Instrument for the Determination of Rain Densities in Flight
Rombus - an Integrated Systems Concept for a Reusable Orbital Module (Booster and Utility Shuttle)
Heat-capacity lag in turbine-working fluids
Flame-visibility Tests with Individual Exhaust Stacks
The Reusable Booster for Lunar Logistics and Planetary Exploration
SLOW-MOTION STUDY Of Injection and Combustion of Fuel In a Diesel Engine
Tests of an Adjustable-area Exhaust Nozzle for Jet-propulsion Engines
ENGINEERING DEVELOPMENT of the JET ENGINE and GAS TURBINE BURNER
Preliminary Study of a Propeller Powered by Gas Jets Issuing from the Blade Tips
EJECTION COOLING OF THE XR-10 HELICOPTER POWER PLANT
Introduction to the problem of rocket-powered aircraft performance
Performance of a Double-row Radial Aircraft Engine with Three Methods of Safety-fuel Injection
Performance of conical jet nozzles in terms of flow and velocity coefficients
Preliminary PERFORMANCE ANALYSIS OF GAS TURBINE POWERPLANTS
Analysis of altitude compensation systems for aircraft carburetors
NUMBERING POSITIONS FOR NOZZLES, BURNERS, ETC. FOR TURBO-JET AND TURBO-PROP ENGINES
Stress Investigations In Gas Turbine Discs and Blades
Equilibrium operating performance of axial-flow turbojet engines by means of idealized analysis
Practical Conclusions on GAS TURBINE SPRAY NOZZLES
Investigation of a Two-step Nozzle in the Langley 11-inch Hypersonic Tunnel
Three-dimensional supersonic nozzles and inlets of arbitrary exit cross section
An Improved System for Control and Measurement of Air Consumption of a Single Cylinder Engine
Exhaust Nozzle Study for MX-1787 Propulsion System
Turbojet-Engine Design Problems for Supersonic Flight
Matching of Auxiliary Inlets to Secondary-Air Requirements of Aircraft Ejector Exhaust Nozzles
Theory of Combustion Instability in Liquid Propellant Rocket Motors