Browse TRAIL Inventories

Analysis of heat addition in a convergent-divergent nozzle

Investigation at supersonic speeds of an inlet employing conical flow separation from a probe ahead of a blunt body

Thrust and Pumping Characteristics of a Series of Ejector-type Exhaust Nozzles at Subsonic and Supersonic Flight Speeds

Thrust and pumping characteristics of a series of ejector-type exhaust nozzles at subsonic and supersonic flight speeds

Investigation of thrust and drag characteristics of a plug-type exhaust nozzle

Thrust and drag characteristics of a convergent-divergent nozzle with various exhaust jet temperatures

Performance of a 16-inch ram-jet engine with a can-type combustor at Mach numbers of 1.50 to 2.16

Application of oblique-shock sensing system to ram-jet-engine flight Mach number control

Matching of auxiliary inlets to secondary-air requirements of aircraft ejector exhaust nozzles

Investigation at supersonic and subsonic Mach numbers of auxiliary inlets supplying secondary air flow to ejector exhaust nozzles

Exhaust Nozzles for Supersonic Flight with Turbojet Engines

Performance comparison at Mach numbers 1.8 and 2.0 of full-scale and quarter-scale translating-spike inlets

Investigation of a supersonic-inlet - turbojet-engine combination at Mach 2.0 and angles of attack up to 6 degrees

Use of main-inlet bypass to supply ejector exhaust nozzle at supersonic speeds

Use of constant diffuser Mach number as a control parameter for variable-geometry inlets at Mach numbers of 1.8 to 2.0

Performance Comparison at Mach Numbers 1.8 and 2.0 of Full Scale and Quarter Scale Translating-Spike Inlets

Use of Constant Diffuser Mach Number as a Control Parameter for Variable-Geometry Inlets at Mach Numbers of 1.8 to 2.0

A performance analysis of methods for handling excess inlet flow at supersonic speeds


Published Year

Subject

Author