WorldCat Identities

Strahle, Warren C.

Overview
Works: 77 works in 126 publications in 1 language and 713 library holdings
Genres: Conference proceedings  Handbooks, manuals, etc 
Roles: Author
Classifications: TL507, 629.108 S
Publication Timeline
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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 222 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 )

2 editions published in 1979 in English and held by 58 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, 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
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
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

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
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

The primary task of this grant was to design, build and check out an acoustics apparatus to measure both audible and ultrasonic acoustic emissions from burning composite solid propellants at pressures to 1000 psia. The check out was achieved with propellants furnished by the Air Force Rocket Propulsion Laboratory. Preliminary results are reported on the acoustic emissions from these propellants in the attachment. The apparatus description is also given in the attachment
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 3 WorldCat member libraries worldwide

Aeroacoustics : jet noise, combustion and core engine noise : technical papers from AIAA 2nd Aero-Acoustics Conference, 1975 by AAIA Aero-Acoustics Specialists Conference( Book )

2 editions 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

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 investigations of fundamentals of rockets and reaction propulsion: (1) Measurement of the dynamic response of solid propellant combustion to flow oscillations, using an impedance tube method. Measurements were made of pressure-coupled combustion response and bulk damping of aluminized and nonaluminized propellants, and the development of an apparatus for measurement of velocity coupled response is near completion; (2) Use of external base burning as a means of producing reduced drag or positive thrust on a supersonic bluff base flight vehicle. Flow field and surface measurements were made in cold flow simulation and in hydrogen fueled tests in a Mach test duct; (3) Combustion of powdered aluminum as a fuel ingredient in solid propellants. A variety of tests were developed and used to clarify and control the agglomeration-combustion behavior of aluminum that usually compromises its effectiveness as a fuel; and (4) Turbulence-generated noise in the interior flow of rocket motors. Measurements were made in cold flow simulators of solid rocket combustors, and results were compared with predictions based on adaptation of the Bernoulli enthalpy theory of aeroacoustics. (Author)
Fractal image compression of Rayleigh, Raman, LIF, and LDV data in turbulent reacting flows by Warren C Strahle( Book )

3 editions published between 1990 and 1991 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 2 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
Experiments Related to External Burning for Propulsion( Book )

3 editions published between 1976 and 1977 in English and held by 2 WorldCat member libraries worldwide

An experimental study of base flows for a 2.25 inch diameter projectile at Mach 3 with cold air injection is reported. Upstream radial jet injection and base injection are used. The work is a continuation of a systematic study of many of the flow field features of external burning. It is shown that radial jet injection alters the wake structure, shortens the wake, and reduces the base pressure. In addition, the advantage of base injection using porous base bleed diminish with injection rate and external compression. (Author)
 
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Alternative Names
Strahle, W. C.

Strahle, W. C. (Warren C.)

Languages
English (57)