#
Aerodynamics, Supersonic
Resource Information
The concept ** Aerodynamics, Supersonic** represents the subject, aboutness, idea or notion of resources found in **Indiana State Library**.

The Resource
Aerodynamics, Supersonic
Resource Information

The concept

**Aerodynamics, Supersonic**represents the subject, aboutness, idea or notion of resources found in**Indiana State Library**.- Label
- Aerodynamics, Supersonic

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- (EG-IN)1251824

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- Wing-alone aerodynamic characteristics for high angles of attack at supersonic speeds
- A computational system for aerodynamic design and analysis of supersonic aircraft : part 1-general description and theoretical development
- A computational system for aerodynamic design and analysis of supersonic aircraft : part 3-computer program description
- A finite difference solution for the propagation of sound in near sonic flows
- A modification to linearized theory for prediction of pressure loadings on lifting surfaces at high supersonic Mach numbers and large angles of attack
- A sensitivity equation approach to shape optimization in fluid flows
- A study of the sonic-boom characteristics of a blunt body at a Mach number of 4.14
- A study of the sonic-boom characteristics of a blunt body at a Mach number of 6
- A wing concept for supersonic maneuvering
- Aerodynamic characteristics of a Sparrow III missile model in the flow field of a generalized parent body at Mach 2.86
- Aerodynamic characteristics of a distinct wing-body configuration at Mach 6 : experiment, theory, and the hypersonic isolation principle
- Aerodynamic characteristics of a fixed arrow-wing supersonic cruise aircraft at Mach numbers of 2.30, 2.70, and 2.95
- Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ÌŠswept double-delta wing at Mach number 0.2
- Aerodynamic characteristics of a supersonic fighter aircraft model at Mach 0.40 to 2.47
- Aerodynamic test and analysis of a turbojet-boosted launch vehicle concept (spacejet) over a Mach number range of 1.50 to 2.86
- An experimental investigation of a Mach 3.0 high-speed civil transport at supersonic speeds
- Analysis and control of asymmetric vortex flows and supersonic vortex breakdown
- Analysis and control of asymmetric vortex flows and supersonic vortex breakdown : final report for the period December 1, 1991 to November 30, 1992
- Analysis and control of supersonic vortex breakdown flows
- Analytical and experimental studies of a short compact subsonic diffuser for a two-dimensional supersonic inlet
- Application of a two-dimensional unsteady viscous analysis code to a supersonic throughflow fan stage
- Application of advanced computational codes in the design of an experiment for a supersonic throughflow fan rotor
- Automatic computation of wing-fuselage intersection lines and fillet inserts with fixed-area constraint
- Body and canard effects on an attached-flow maneuver wing at Mach 1.62
- Bumblebee Program - aerodynamic data
- Calculation of aerodynamic heat transfer for blunt-nosed thin wings at different angles of attack at supersonic speeds
- Calculation of subsonic and supersonic steady and unsteady aerodynamic forces using velocity potential aerodynamic elements
- Calculation of three-dimensional, inviscid supersonic, steady flows
- Coherent large-scale structures in high Reynolds number supersonic jets
- Computation of separation ahead of blunt fin in supersonic turbulent flow
- Correlations of supersonic boundary-layer transition on cones including effects of large axial variations in wind-tunnel noise
- Design and demonstration of a system for routine, boomless supersonic flights
- Development of a computer code for calculating the steady super/hypersonic inviscid flow around real configurations : volume II - code description
- Development of supersonic computational aerodynamic program using panel method
- Development of the triplet singularity for the analysis of wings and bodies in supersonic flow
- Effect of Reynolds number on the aerodynamic stability and control characteristics of a 55 degree clipped-delta-wing orbiter configuration at supersonic Mach numbers
- Effect of leading-edge load constraints on the design and performance of supersonic wings
- Effect of planform and body on supersonic aerodynamics of multibody configurations
- Effect on tail-fin span on stability and control characteristics of a canard-controlled missile at supersonic Mach numbers
- Effects of forebody strakes and Mach number on overall aerodynamic characteristics on configuration with 550 cropped delta wing
- Effects of roughness size on the position of boundary-layer transition and on the aerodynamic characteristics of a 55 ÌŠswept delta wing at supersonic speeds
- Effects of spanwise nozzle geometry and location on the longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration at subsonic speeds
- Engineering supersonic aerodynamics
- Estimation of wing nonlinear aerodynamic characteristics at supersonic speeds
- Euler flow predictions for an oscillating cascade using a high resolution wave-split scheme
- Evaluation of a technique to generate artificially thickened boundary layers in supersonic and hypersonic flows
- Experimental aerodynamic characteristics at Mach numbers from 0.60 to 2.70 of two supersonic cruise fighter configurations
- Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63
- Experimental and theoretical supersonic lateral-directional stability characteristics of a simplified wing-body configuration with a series of vertical-tail arrangements
- Experimental cavity pressure distributions at supersonic speeds
- Experimental effects of wing location on wing-body pressures at supersonic speeds
- Experimental investigation of leading-edge thrust at supersonic speeds
- Experimental investigation of porous-floor effects on cavity flow fields at supersonic speeds
- Experimental investigation to validate use of cryogenic temperatures to achieve high Reynolds numbers in boattail pressure testing
- Extension of multigrid methodology to supersonic/hypersonic 3-D viscous flows
- Flight test results of riblets at supersonic speeds
- Fluctuating loads measured on an over-the-wing supersonic jet model
- Influence of airfoil geometry on delta wing leading-edge vortices and vortex-induced aerodynamics at supersonic speeds
- Inlet flowfield investigation, Part II, Computation of the flow about a supercruise forebody at supersonic speeds.
- Interference effects of aft reaction-control yaw jets on the aerodynamic characteristics of a space shuttle orbiter model at supersonic speeds
- Investigation of convergent-divergent nozzles applicable to reduced-power supersonic cruise aircraft
- Investigation of flow characteristics over missle bodies at supersonic speeds
- Investigation of leading-edge flap performance on delta and double-delta wings at supersonic speeds
- Longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration at subsonic speeds
- Longitudinal and lateral-directional aerodynamic characteristics of a wing-cone configuration at Mach numbers from 2.5 to 4.5
- Low-speed aerodynamic characteristics of a highly swept, untwisted, uncambered arrow wing
- Low-speed static and dynamic force tests of a generic supersonic cruise fighter configuration
- Mechanical property characterization of BorsicÂ®/aluminum laminates at room and elevated temperatures
- Navier-Stokes and Euler solutions for lee-side flows over supersonic delta wings : a correlation with experiment
- Nonaxisymmetric viscous lower branch modes in axisymmetric supersonic flows
- Nonlinear potential analysis techniques for supersonic/hypersonic aerodynamic design
- Nonparallel instability of supersonic and hypersonic boundary layers
- Numerical analysis of supersonic flow through oscillating cascade sections by using a deforming grid
- Numerical simulation of steady supersonic viscous flow
- Numerical simulations of supersonic flow through oscillating cascade sections
- PAN AIR, a computer program for predicting subsonic or supersonic linear potential flows about arbitrary configurations using a higher order panel method
- Planform effects on the supersonic aerodynamics of multibody configurations
- Prediction of vortex shedding from circular and noncircular bodies in supersonic flow
- Pressure and force data for a flat wing and a warped conical wing having a shockless recompression at Mach 1.62
- Pressure data for four analytically defined arrow wings in supersonic flow
- Progress in supersonic cruise aircraft technology
- Propulsion and airframe aerodynamic interactions of supersonic V/STOL configurations
- Review of aeronautical wind tunnel facilities
- Screech noise source structure of a supersonic rectangular jet
- Secondary instability of high-speed flows and the influence of wall cooling and suction
- Semi-annual status report on NASA grant NSG 1629 "An investigation of vortex-induced aerodynamic characteristics of supersonic cruise configurations" : July 1, 1984 - December 31, 1984
- Shock capturing finite difference algorithms for supersonic flow past fighter and missile type configurations
- Some observations on a new numerical method for solving the Navier-Stokes equations
- Spectral methods for modeling supersonic chemically reacting flow fields
- Statistical model of sonic boom structural damage
- Steady and nonsteady supersonic turbulent afterbody flow
- Study of lee-side flows over conically cambered delta wings at supersonic speeds
- Study of supersonic wings employing the attainable leading-edge thrust concept
- Supersonic aerodynamic characteristics of a proposed assured crew return capability (ACRC) lifting-body configuration
- Supersonic aerodynamic characteristics of a series of wrap-around-fin missile configurations
- Supersonic aerodynamic characteristics of a space shuttle orbiter model at angles of attack from 200 to 900
- Supersonic aerodynamic characteristics of an advanced F-16 derivative aircraft configuration
- Supersonic aerodynamic characteristics of some reentry concepts for angles of attack to 900
- Supersonic aerodynamics of delta wings
- Supersonic axial-force characteristics of a rectangular-box cavity with various length-to-depth ratios in a flat plate
- Supersonic combustion engine testbed : heat lightning
- Supersonic nonlinear potential flow analysis : interim report
- Supersonic reacting internal flow fields
- Supersonic stability and control characteristics of a cruciform missile model with delta wings and aft tail fin controls
- Supersonic through-flow fan design
- Supersonic wings with significant leading-edge thrust at cruise
- Supersonic, nonlinear, attached-flow wing design for high lift with experimental validation
- Surface pressure data for a supersonic-cruise airplane configuration at mach numbers of 2.30, 2.96, and 3.30
- Surface pressure data on a series of analytic forebodies at Mach numbers from 1.70 to 4.50 and combined angles of attack and sideslip
- Surface pressure data on a series of conical forebodies at mach numbers from 1.70 to 4.50 and combined angles of attack and sideslip
- Survey and analysis of research on supersonic drag-due-to-lift minimumization with recommendations for wing design
- Systematic study of error sources in supersonic skin-friction balance measurements
- Tables of supersonic flow around cones of large yaw
- The aerodynamic design of the oblique flying wing supersonic transport
- The natural flow wing-design concept
- The predicted effect of aerodynamic detuning of coupled bending-torsion unstalled supersonic flutter
- The separation of supersonic flow from curved profiles
- The wedge hot-film anemometer in supersonic flow
- Theoretical and experimental engine-inlet flow fields for fighter forebodies
- Theoretical and experimental investigation of supersonic aerodynamic characteristics of a twin-fuselage concept
- Theoretical evaluation of high-speed aerodynamics for arrow-wing configurations
- Transonic and supersonic Euler computations of vortex-dominated flow fields about a generic fighter
- Unsteady flow in a supersonic cascade with two in-passage shocks
- User's guide to a system of finite-element supersonic panel flutter programs
- Velocity field of a round jet in a cross flow for various jet injection angles and velocity ratios
- Viscous flow simulations of internal store carriage and separation : final report for the period ended May 15, 1991
- Wave-interactions in supersonic and hypersonic flows
- Wind-tunnel investigation at supersonic speeds of a canard-controlled missile with fixed and free-rolling tail fins
- Wind-tunnel investigation at supersonic speeds of a remote-controlled canard missile with a free-rolling-tail brake torque system
- Wind-tunnel/flight correlation study of aerodynamic characteristics of a large flexible supersonic cruise airplane (XB-70-1)
- Wing planform effects at supersonic speeds for an advanced fighter configuration
- A System for aerodynamic design and analysis of supersonic aircraft

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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/Th_kFszVVNY/" 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/Th_kFszVVNY/">Aerodynamics, Supersonic</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>`