Jet nozzles
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The concept Jet nozzles represents the subject, aboutness, idea or notion of resources found in Indiana State Library.
The Resource
Jet nozzles
Resource Information
The concept Jet nozzles represents the subject, aboutness, idea or notion of resources found in Indiana State Library.
- Label
- Jet nozzles
- Authority link
- (EG-IN)1355811
64 Items that share the Concept Jet nozzles
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- Viscous three-dimensional analyses for nozzles for hypersonic propulsion
- A nozzle internal performance prediction method
- Acoustic and aerodynamic performance investigation of inverted velocity profile connualar plug nozzles
- Acoustic, performance, and wake survey measurements of a lobed velocity-decayer nozzle installed on a quieted TF-34 turbofan engine
- Aeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20
- Aeropropulsive characteristics of nonaxisymmetric-nozzle thrust reversers at Mach numbers from 0 to 1.20
- Aeropulsive characteristics at Mach numbers up to 2.2 of axisymmetric and nonaxisymmetric nozzles installed on an F-18 model
- Aircraft ground test and subscale model results of axial thrust loss caused by thrust vectoring using turning vanes
- Alternate nozzle ablative materials program : final report covering period October 11, 1982 to May 21, 1983
- An experimental investigation of thrust vectoring two-dimensional convergent-divergent nozzles installed in a twin-engine fighter model at high angles of attack
- An improved analytical model of the separation region on boattail nozzles at subsonic speeds
- Analysis and optimization of truncated scarf nozzles subject to external flow conditions
- Boundary-layer separation on isolated boattail nozzles
- Divergence thrust loss calculations for convergent-divergent nozzles : extensions to the classical case
- Effect of 'delta tabs' on mixing and axis switching in jets from asymmetric nozzles
- Effect of a trade between boattail angle and wedge size on the performance of a nonaxisymmetric wedge nozzle
- Effect of initial tangential velocity distribution on the mean evolution of a swirling turbulent free jet
- Effect of jet exit vanes on flow pulsations in an open-jet wind tunnel
- Effect of nozzle and vertical-tail variables on the performance of a three-surface F-15 model at transonic Mach numbers
- Effect of thrust reverser operation on the lateral-directional characteristics of a three-surface F-15 model at transonic speeds
- Effect of thrust vectoring and wing maneuver devices on transonic aeropropulsive characteristics of a supersonic fighter aircraft
- Effects of installation of F101 DFE exhaust nozzles on the afterbody-nozzle characteristics of the F-14 airplane
- Effects of internal yaw-vectoring devices on the static performance of a pitch-vectoring nonaxisymmetric convergent-divergent nozzle
- Effects of sidewall geometry on the installed performance of nonaxisymmetric convergent-divergent exhaust nozzles
- Effects of twin-vertical-tail parameters on twin-engine afterbody/nozzle aerodynamic characteristics
- Evaluation of flip-flop jet nozzles for use as practical excitation devices
- Evaluation of water cooled supersonic temperature and pressure probes for application to 2000F̊ flows
- Experimental and analytical investigation of a nonaxisymmetric and wedge nozzle at static conditions
- Experimental investigation of nozzle/plume aerodynamics at hypersonic speeds
- Experimental investigation of shock-cell noise reduction for dual-stream nozzles in simulated flight
- Experimental investigation of shock-cell noise reduction for single-stream nozzles in simulated flight : comprehensive data report
- Experimental investigation of the effects of aft blowing with various nozzle exit geometries on a 3.0 caliber tangent Ogive at high angles of attack : forebody pressure distributions
- Experimental investigation of two nonaxisymmetric wedge nozzles at free-stream Mach numbers up to 1.20
- Experimental research of the aerodynamics of nozzles and plumes at hypersonic speeds
- Experimental results for a two-dimensional supersonic inlet used as a thrust deflecting nozzle
- Experimental results of a deflected thrust V/STOL nozzle research program
- Flow visualization and interpretation of visualization data for deflected thrust V/STOL nozzles
- Free jet feasibility study of a thermal acoustic shield concept for AST/VCE application : dual stream nozzles
- Free jet feasibility study of a thermal acoustic shield concept for AST/VCE application : single stream nozzles
- Free-jet investigation of mechanically suppressed, high-radius-ratio coannular plug model nozzles
- Full Navier-Stokes analysis of a two-dimensional mixer/ejector nozzle for noise suppression
- Internal pressure distributions for a two-dimensional thrust-reversing nozzle operating at a free-stream mach number of zero
- Jet engine hot parts IR analysis procedure (J-EIRP)
- Mixing and noise benefit versus thrust penalty in supersonic jets using impingement tones
- Numerical method for predicting flow characteristics and performance of nonaxisymmetric nozzles : part 2 - applications
- Numerical method for predicting flow characteristics and performance of nonaxisymmetric nozzles : theory
- Operating characteristics of the multiple critical venturi system and secondary calibration nozzles used for weight-flow measurements in the Langley 16-foot transonic tunnel
- Parametric experimental investigation of a scramjet nozzle at Mach 6 with freon and argon or air used for exhaust simulation
- Parametric study of afterbody/nozzle drag on twin two-dimensional convergent-divergent nozzles at mach numbers from 0.60 to 1.20
- Performance characteristics of an isolated coannular plug nozzle at transonic speeds
- Performance characteristics of axisymmetric convergent-divergent exhaust nozzles with longitudinal slots in the divergent flaps
- Performance of twin-dimensional wedge nozzles including thrust vectoring and reversing effects at speeds up to Mach 2.20
- Pressures measured in flight on the aft fuselage and external nozzle of a twin-jet fighter
- Refinement and application of acoustic impulse technique to study nozzle transmission characteristics
- Static and wind tunnel near-field/far-field jet noise measurements from model scale single-flow baseline and suppressor nozzles : summary report
- Static internal performance of a single expansion ramp nozzle with multiaxis thrust vectoring capability
- Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap
- Static internal performance of a two-dimensional convergent-divergent nozzle with thrust vectoring
- Static internal performance of ventral and rear nozzle concepts for short-takeoff and vertical-landing aircraft
- Static investigation of a two-dimensional convergent-divergent exhaust nozzle with multiaxis thrust-vectoring capability
- Supersonic jets from bevelled rectangular nozzles
- Thermal/structural analysis of a transpiration cooled nozzle
- User's guide for the NOZL3D and NOZLIC computer programs
- Viscous computations of cold air/airflow around scramjet nozzle afterbody
- Viscous flow simulations of internal store carriage and separation : final report for the period ended May 15, 1991
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<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.library.in.gov/resource/DdG322I8NpU/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.library.in.gov/resource/DdG322I8NpU/">Jet nozzles</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.library.in.gov/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.library.in.gov/">Indiana State Library</a></span></span></span></span></div>
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<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.library.in.gov/resource/DdG322I8NpU/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.library.in.gov/resource/DdG322I8NpU/">Jet nozzles</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.library.in.gov/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.library.in.gov/">Indiana State Library</a></span></span></span></span></div>
