WorldCat Identities

Strahle, Warren C.

Overview
Works: 77 works in 126 publications in 1 language and 709 library holdings
Genres: Conference proceedings  Handbooks, manuals, etc 
Roles: Author
Classifications: TL507, 629.108 S
Publication Timeline
Key
Publications about  Warren C Strahle Publications about Warren C Strahle
Publications by  Warren C Strahle Publications by Warren C Strahle
Most widely held works by Warren C Strahle
Aeroacoustics : technical papers from AIAA 2nd Aero-acoustics Conference, March 1975, subsequently revised for this volume by AIAA Aero-acoustics Conference ( Book )
4 editions published in 1976 in English and held by 229 WorldCat member libraries worldwide
An introduction to combustion by Warren C Strahle ( Book )
9 editions published between 1993 and 1996 in English and held by 173 WorldCat member libraries worldwide
Combustion noise prediction, entropy/vorticity effects ( Book )
4 editions published in 1979 in English and held by 59 WorldCat member libraries worldwide
Aeroacoustics, fan noise and control, duct acoustics, rotor noise : technical papers from AIAA 2nd Aero-acoustics Conference, March 1975, subsequently revised for this volume by AIAA Aero-acoustics Conference ( Book )
2 editions published in 1976 in English and held by 40 WorldCat member libraries worldwide
"The recent progress in duct acoustic research is reflected by fourteen papers which cover essentially the areas of linear duct acoustics, the characteristics of absorbent materials, and nonlinear duct acoustics. With respect to propagation in ducts, emphasis is placed on computational methods aimed at attaining effective economical modeling of propagation in variable-geometry and in hard-wall or soft-wall ducts. Computational methods developed to reduce computer processing and storage requirements are outlined, along with a wave envelope technique for reducing processing and storage needs. The latter technique is applied to the optimum segmented acoustic duct linear design. A finite difference technique is used in combination with conformal mapping to compute the optimum multisection duct linear design."--Publisher description
Aeroacoustics, acoustic wave propagation, aircraft noise prediction, aeroacoustic instrumentation : technical papers from AIAA 2nd Aero-acoustics Conference, March 1975, subsequently revised for this volume by AIAA Aero-Acoustics Specialists Conference ( Book )
2 editions published in 1976 in English and held by 38 WorldCat member libraries worldwide
"The papers in this volume deal with recent research into acoustic-wave propagation through the atmosphere and progress in aeroacoustic instrumentation, facilities, and test techniques. Topics include the propagation of aircraft noise over long distances in the lower atmosphere, measured effects of turbulence on the rise time of a weak shock, sound scattering from atmospheric turbulence, saturation effects associated with sound propagation in a turbulent medium, and a computer model of the lightning-thunder process. Other papers discuss the development of a computer system for aircraft noise prediction; aircraft flyover noise measurements; and theories and methods for the prediction of ground effects on aircraft noise propagation, for the prediction of airframe aerodynamic noise, for turbine noise prediction, and for combustion noise prediction. Attention is also given to the use of Hartmann generators as sources of high-intensity sound in a large absorption flow-duct facility, an outdoor jet noise facility, factors in the design and performance of free-jet acoustic wind tunnels, and the use of a laser shadowgraph for jet noise diagnosis."--Publisher description
Aeroacoustics, STOL noise, airframe and airfoil noise : technical papers from AIAA 2nd Aero-acoustics Conference, March 1975, subsequently revised for this volume by AIAA Aero-acoustics Conference ( Book )
2 editions published in 1976 in English and held by 38 WorldCat member libraries worldwide
"The papers in this volume reflect the progress in aeroacoustic research which has been made in the field of VTOL and V/STOL aircraft noise. The research was directed mainly at developing better methods for predicting noise generation and propagation, at determining the effects of pressure fluctuations on surfaces and interior noise, and at developing noise abatement techniques. Among the topics covered are: scrubbing noise of externally blown flaps; propulsive-lift noise of an upper-surface-blown flap configuration; the aeroacoustic characteristics of model slot nozzles with straight flaps; fluctuating pressures on aircraft wing and flap surfaces associated with powered-lift systems; acoustic characteristics of a large upper-surface-blown configuration with turbofan engines; the effect of forward speed on jet/flap interaction noise; and airframe noise in the far field."--Publisher description
A theoretical study of unsteady droplet burning : transients and periodic solutions by Warren C Strahle ( )
5 editions published between 1963 and 1964 in English and held by 7 WorldCat member libraries worldwide
The computation of oblique shock wave characteristics for real gases by Warren C Strahle ( Book )
1 edition published in 1961 in English and held by 6 WorldCat member libraries worldwide
The thermodynamic properties and shock-wave characteristics of a model Venus atmosphere by Warren C Strahle ( Book )
1 edition published in 1962 in English and held by 5 WorldCat member libraries worldwide
Audible and Ultrasonic Acoustic Emissions from Composite Solid Propellants ( Book )
4 editions published between 1975 and 1977 in English and held by 4 WorldCat member libraries worldwide
An apparatus to test the audible and ultrasonic emissions from composite solid propellants was designed, constructed and checked out. Tests were conducted at 300 psia for eight aluminized HTPB-AP propellants. The tests were conducted under both nitrogen and air pressurization. For the audible emissions in the range 100 - 2500 Hz there is a marked effect of the pressurization fluid. In air the noise output is 10,000 higher than in nitrogen. There is a definite possibility that the noise output is responsible for observed chamber pressure roughness level. For the ultrasonic signal in the range 50 to 300 kHz there are strong spectral peaks observed but their origin is not clear and they do not correlate with observed deflagration behavior. For audible signals a striking effect of AFCAM aluminum coating is the reduction of signal strength
Heterogeneous Diffusion Flame Stabilization by Warren C Strahle ( Book )
4 editions published in 1987 in English and held by 4 WorldCat member libraries worldwide
Analytical modelling and several experimental diagnostics were applied to an experimental flow in a two-dimensional subsonic windtunnel with a backward facing step and provision for injection of inerts and combustibles through the porous floor behind the step. The analytical techniques were based on a two equation modeling of turbulence with several variants of near wall models and numerical approaches. Conventional experimental techniques, where applicable in the cold flow, included hot film and pitot and anemometry. Laser - based diagnostics in the cold and hot flows for velocity and species concentration measurements (both mean and instantaneous) included laser velocimetry in two components and Rayleigh molecular scattering. Major findings in this complex turbulent flow with chemical reactions were a) there was a general agreement between analysis and experiment in cold flow both with and without wall injection, b) this agreement occurred at the the most detailed level of turbulent shear stress and mass transport, c) in hot flow there was acceptable agreement as to the gross features of the mean flow field, but some theoretical details, such as reattachment length, went counter to experimental results
Aeroacoustics: jet noise, combustion and core engine noise : technical papers from AIAA 2nd Aero-Acoustics conference : (Hampton - Va.), March 1975 by AAIA Aero-Acoustics Specialists Conference ( Book )
2 editions published in 1976 in English and held by 4 WorldCat member libraries worldwide
Aeroacoustics: STOL noise : airframe and airfoil noise : technical papers from AIAA 2nd Aero-Acoustics conference : (Hampton - Va.), March 1975 ( Book )
2 editions published in 1976 in English and held by 4 WorldCat member libraries worldwide
Rocket Research at Georgia Tech ( Book )
3 editions published between 1979 and 1981 in English and held by 3 WorldCat member libraries worldwide
Progress is reported on four distinct projects which are administered as a group. The individual projects are identified as tasks and reported on separately. A summary for each task follows: Task I. Work concerned improvement and application of the impedance tube method for measurement of the presure-coupled combustion response of solid propellants and measurement of the bulk damping in the product flow. Improvements included increaed sites and amplitude range of pressure measurements; increased capacity of the data acquisition system; and a modified, more rapid data reduction program. Admittances and bulk loss coefficients of nonaluminized and aluminized propellants were measured over a range of frequencies. Task II. Studies were continued on external burning using an axisymmetric model at Mach 3. Tests with actual combustion of radially and axially injected hydrogen are then reported. Outstanding performance values with significant base drag reduction is shown for injection and burning directly in the near-wake (base burning). Task III. Investigations continued of the accumulation processes of aluminum on the propellant burning surface that lead to formation of agglomerate droplets, the size of which dominates aluminum combustion. Task IV. Experimental and analytical studies were continued on the subject of turbulence-induced pressure fluctuations in a rocket-like cavity. A new theory was constructed for the generation of pressure disturbances by the turbulence. Undeniable separation has been achieved between propagational and local pressure fluctuations, and the agreement between theory and experiment are adequate
Aeroacoustics: Acoustic Wave Propagation; Aircraft Noise Prediction; Aeroacoustic Instrumentation ( )
1 edition published in 1976 in English and held by 3 WorldCat member libraries worldwide
Acoustic Signature from Flames as a Combustion Diagnostic Tool by Warren C Strahle ( Book )
3 editions published in 1983 in English and held by 3 WorldCat member libraries worldwide
A program was conducted to investigate the feasibility of using the combustion noise acoustic output as a non-intrusive diagnostic of some details of the combustion process. Investigated were an open premixed turbulent jet flame and a gas turbine combustor converted to run on propane. The analysis links the acoustic pressure fluctuations to the distribution of heat release rate fluctuations. Measurement of the sound field, yields in principle, the heat release rate fluctuation field. It was found, however, that the analytical methods for this inverse problem are too sensitive to small experimental uncertainties. Consequently, it appears that the method is not, in general feasible
Aeroacoustics: Fan Noise and Control; Duct Acoustics; Rotor Noise ( )
1 edition published in 1976 in English and held by 3 WorldCat member libraries worldwide
Aeroacoustics : technical papers from AIAA 2nd Aero-Acoustics Conference, March 1975, subsequently revised for this volume ( Book )
1 edition published in 1976 in English and held by 3 WorldCat member libraries worldwide
 
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Audience level: 0.79 (from 0.00 for Audible an ... to 1.00 for The thermo ...)
Alternative Names
Strahle, W. C.
Strahle, W. C. (Warren C.)
Languages
English (55)