Aerodynamic Loads on an Isolated Shrouded-propeller Configuration for Angles of Attack from -10 Deg to 110 Deg
Aerodynamic loads on an isolated shrouded- propeller configuration for various angles of attack
AERODYNAMIC LOAD↗
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PERFORMANCE CHARACTERISTICS OF SEVERAL DIVERGENT-SHROUD AIRCRAFT EJECTORS
Performance characteristics of several divergent- shroud aircraft ejectors
EJECTOR↗
Performance of a variable divergent-shroud ejector nozzle designed for flight mach numbers up to 3.0
Pumping and internal thrust performance of simulated variable divergent-shroud ejector nozzle designed for flight Mach numbers to 3.0
SHROUDED NOZZLE↗
Characteristics of supersonic ejector systems with nonconstant area shroud.
Aircraft supersonic ejector system with nonconstant area shroud stressing inviscid and viscid interaction between primary and secondary streams
SHROUDED BODY↗
Transmission of sound and vibration to a shroud-enclosed spacecraft
Statistical energy analysis for predicting sound and vibration transmission in shroud-enclosed spacecraft
VIBRATION↗
Comparison of the Agena/Mariner-C and Agena/Lunar orbiter shroud aerodynamic characteristics for the Mach number range from 0.56 to 3.46
Models of Agena/Mariner C and Agena/Lunar Orbiter shroud tested in wind tunnels over Mach number range 0.56 to 3.46 for comparison of aerodynamic characteristics
MARINER C PROGRAM↗
Investigation of HF and VHF Rocket-borne Shroud Antennas
High frequency and very high frequency rocketborne shroud antennas
ANTENNA↗
Fabrication of lightweight turbine components using electron-beam welding for the attachment of sheet metal blades to discs and shrouds
Fabrication of lightweight turbine components for M-1 engine oxidizer turbopump using electron beam welding for attaching sheet metal blades to discs and shrouds
TURBOPUMP↗
Materials in an Atlas-Agena shroud.
Shroud for Lunar Orbiter atop Atlas-Agena launch vehicle, noting structural alloys used
STRUCTURAL MATERIAL↗
Voyager spacecraft phase B, task D. Volume 10 - Engineering study tasks - Shroud, temperature control, plume heating Final report
Engineering analysis of shroud, temperature control, and plume heating in recommended Voyager spacecraft configuration
Source record↗
Fabrication techniques for shrouded titanium impeller Quarterly progress report, period ending 31 Mar. 1968
Fabrication techniques for shrouded titanium impeller
Edlebeck, N. A.↗
Development of a liquid shroud cryogenic supercritical pressure storage system
Liquid shroud cryogenic supercritical pressure storage system for space applications
Source record↗
Fabrication techniques for shrouded titanium impeller Quarterly progress report, period ending 31 Dec. 1967
Detailed design drawings and bonding techniques for shrouded titanium impeller
Edlebeck, N. A.↗
Experimental study of sound and vibration transmission to a shroud-enclosed spacecraft Annual report, 20 Jan. 1967 - 20 Jan. 1968
Acoustic and mechanical vibration transmission paths to shroud enclosed spacecraft
Koronaios, N.↗
Performance of a collapsible plug nozzle having either two-position cylindrical or variable angle floating shrouds at Mach numbers from 0 to 2.0
Effects of shroud geometry on performance of collapsible plug nozzle at Mach numbers from 0 to 2.0
Harrington, D. E.↗
Performance characteristics of spiral-groove and shrouded Rayleigh step profiles for high- speed noncontacting gas seals.
Noncontacting gas seals investigated for performance characteristics of spiral groove and shrouded Rayleigh step profiles
Castelli, V.↗
Experimental investigation of a 10 deg conical turbojet plug nozzle with iris primary and translating shroud at Mach numbers from 0 to 2.0
Performance of 10 deg conical turbojet plug nozzle with iris primary and translating shroud for supersonic cruise applications
Bresnahan, D. L.↗
Development of an SPS/DPS Hydrogen Shrouded Cryogenic Helium Storage System Final Report, Jul. 1967 - Sep. 1968
Development of SPS/DPS hydrogen shrouded cryogenic helium storage system
Bald, W. B.↗