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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.

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At least 1,243 records · Page 69

All sources NASA NTRS DOE OSTI

NASA NTRS1969

Investigation of two-phase hydrogen flow in pump inlet line

Two phase hydrogen flow in pump inlet line

Connelly, R. E.↗

NASA NTRS1969

Characteristic design study of mixed- compression two-dimensional inlets with low-angle cowls for the Mach number range 2.70 to 1.80

Design effects on performance of two dimensional mixed-compression supersonic inlets with low angle cowls

Anderson, B. H.↗

NASA NTRS1969

Dynamic response of a Mach 2.5 axisymmetric inlet with engine or cold pipe and utilizing 60 percent supersonic internal area contraction

Dynamic response of supersonic mixed compression inlet coupled to cold pipe or turbojet engine

Wasserbauer, J. F.↗

NASA NTRS1969

A numerical analysis of the use of perforated walls to control shock location and movement in an internal compression supersonic inlet

Numerical analysis of shock control by using perforated walls in internal compression supersonic inlets

Matthews, C. W.↗

NASA NTRS1969

Simplified Analytical Model for Use in Design of Pump-Inlet Accumulators for the Prevention of Liquid-Rocket Longitudinal Oscillation (POGO)

Analytical model for use in design of pump inlet accumulators for prevention of liquid rocket longitudal oscillation

Lewis, William↗

NASA NTRS1969

Internal thrust and pumping performance of an auxiliary inlet ejector nozzle with clamshell thrust reverser

Simulated take-off, transonic acceleration, and supersonic flight conditions using auxiliary inlet ejector nozzle

Burley, R. R.↗

NASA NTRS1969

Reingestion characteristics and inlet flow distortion of V/STOL lift-engine fighter configurations.

Exhaust gas reingestion and inlet flow distortion in V/STOL lift engines, discussing static and wind tunnel testing using fighter configuration models

Barrack, J. P.↗

NASA NTRS1969

Supersonic wind tunnel investigation of inlet- engine compatibility.

Inlet produced dynamic distortion and effects on stall margin of J-85 turbojet engine from supersonic wind tunnel tests

Calogeras, J. E.↗

NASA NTRS1969

A two-dimensional, mixed-compression inlet system designed to self-restart at a Mach number of 3.5.

M 3.5 two dimensional mixed compression inlet system with self restart using flexible variable ramp system

Anderson, W. E.↗

NASA NTRS1969

Study of a family of supersonic inlet systems.

Large scale axisymmetric inlet systems performance capabilities, reviewing theoretical and experimental programs

Cubbison, R. W.↗

NASA NTRS1969

Inlet effects on boiling and near critical hydrogen heat transfer.

Hydrodynamic inlet conditions effect on film boiling and near critical hydrogen heat transfer, using data from electrically heated various geometry test sections

Brown, D. D.↗

NASA NTRS1969