Accession Number : ADA302114

Title :   Short-Term Propulsion and Power Development Analysis/Assessment and Information Dissemination - (UTC).

Descriptive Note : Final rept. 20 Jul 90-17 Jun 95,

Corporate Author : UNIVERSAL TECHNOLOGY CORP DAYTON OH

Personal Author(s) : Bethel, Howard

PDF Url : ADA302114

Report Date : JUN 1995

Pagination or Media Count : 29

Abstract : This final repon documents a summary of all technical accomplishments in performance of the contract "Short-Term Propulsion & Power Development analysis Assessment and information Dissemination" (Contract Fl36l5-90C-2O3l) in support of the Aero Propulsion and power Directorate, Wright Laboratory, Air Force Materiel Command, Wright-Patterson AFB OH. Work accomplished under this contract was documented by Universal Technology Corporation (UTC) as Project SA77. Individual tasks were identified as Project 5477-01 through Project S477-50. The various tasks accomplished under this contract covered a wide variety of teclmical fields and areas of study. Examples include polymer battery research, analysis of the operation of the Compressor Research Facility, an assessment of the integrated High Performance Turbine Engine Technology (lHPTET) Program a drag analysis of a variable flow ducted rocket (VFDR) using the Aerodynamic Preliminary Analysis System (APAS) computer codes, evaluation of Russian scramjet technology and test facilities, test and data reduction procedures for single tube MCH endothermic heat exchanger experiments, generation of residual stress in fan blades using the laser shock peening process, on-site support for the biannual turbine Steering committee meetings, the biennial Turbine Engine Technology Symposium, analyses on combined cycle engnes, NASP flowpath antithermal loads and sing le crystal sheet material for high temperature environments.

Descriptors :   *PROPULSION SYSTEMS, *TURBINE ENGINES, COMPUTER PROGRAMS, USSR, AIR FORCE, MATERIEL, SYMPOSIA, CONTRACTS, INFORMATION TRANSFER, MATERIALS, HEAT EXCHANGERS, RESEARCH FACILITIES, FAN BLADES, LASERS, VARIABLES, SHORT RANGE(TIME), SHOCK, SHEETS, RESIDUAL STRESS, DATA REDUCTION, TURBINES, POWER, FLOW, COMPRESSORS, DRAG, SUPERSONIC COMBUSTION RAMJET ENGINES, TEST FACILITIES, TUBES, ENDOTHERMIC REACTIONS, SHOT PEENING, DUCTED ROCKETS.

Subject Categories : Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE