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SAE ARP1257 - GAS TURBINE ENGINE TRANSIENT PERFORMANCE PRESENTATION FOR DIGITAL COMPUTER PROGRAMS Organization: SAE
Date: 1989-10-20
Description: This Aerospace Recommended Practice provides a method for the presentation of gas turbine engine transient performance as calculated by means of digital computer programs and is compatible with AS681, Gas Turbine Engine Steady-State Performance Presentation for Digital Computer Programs.
SAE AS681 - (R) GAS TURBINE ENGINE PERFORMANCE PRESENTATION FOR COMPUTER PROGRAMS Organization: SAE
Date: 2016-06-01
Description: This SAE Aerospace Standard (AS) provides the method for presentation of gas turbine engine steady-state and transient performance calculated using computer programs.
NPFC - DI-TMSS-81515 - USER’S MANUAL FOR GAS TURBINE ENGINE STEADY-STATE AND TRANSIENT PERFORMANCE PRESENTATION FOR DIGITAL COMPUTER PROGRAMS Organization: NPFC
Date: 2015-05-19
Description: Use/relationship: This Data Item Description (DID) provides the method for presentation of gas turbine engine calculated steady-state and transient performance using computer programs.
SAE ARP4148 - GAS TURBINE ENGINE REAL TIME PERFORMANCE MODEL PRESENTATION Organization: SAE
Date: 2015-03-01
Description: This SAE Aerospace Recommended Practice (ARP) provides guidance for the presentation of gas turbine engine transient performance models with the capacity to be implemented as computer programs operating in real time and is intended to complement AS681.
CTA - EIA REC 141 - VHF RECEIVING PERFORMANCE PRESENTATION & MEASUREMENT Organization: CTA
BSI - BS 1586 - PERFORMANCE TESTING AND PRESENTATION OF PERFORMANCE DATA FOR REFRIGERANT CONDENSING UNITS Organization: BSI
Date: 1982-08-31
Description: Applies to air and water cooled condensing units employing single stage refrigerant compressors including hermetic, semi-hermetic and open types. Describes the method for presentation of performance data for these units including correction factors and part load characteristics where applicable.
CTA-774 - TV RECEIVING ANTENNA PERFORMANCE PRESENTATION MEASUREMENT - FORMERLY ANSI/CEA-774-C Organization: CTA
Date: 2014-11-01
Description: Essential elements include procedures to determine antenna gain, front-to-back ratio, average gain to null ratio, directivity and distortion performance of active antennas with integrated amplifiers.
SAE ARP1211 - GAS TURBINE ENGINE STATUS PERFORMANCE PRESENTATION FOR DIGITAL COMPUTER PROGRAMS Organization: SAE
Date: 1993-05-01
SAE AS18 - PERFORMANCE PRESENTATION, AIRCRAFT RECIPORCATING ENGINE - TWO SPEED ENGINE Organization: SAE
Date: 2004-07-15
SAE AS19 - PERFORMANCE PRESENTATION, AIRCRAFT RECIPROCATING ENGINE - ENGINE STAGE ENGINE Organization: SAE
Date: 2004-07-15
SAE AS16 - PERFORMANCE PRESENTATION, AIRCRAFT RECIPROCATING ENGINE - SINGLE SPEED ENGINE Organization: SAE
Date: 2004-07-15
SAE AS17 - PERFORMANCE PRESENTATION, AIRCRAFT RECIPROCATING ENGINE - TWO SPEED ENGINE Organization: SAE
Date: 2004-07-15
BSI - BS 6019 - RECOMMENDATIONS FOR PERFORMANCE STANDARDS IN BUILDINGS: CONTENTS AND PRESENTATION Organization: BSI
Date: 1980-12-31
Description: Gives recommendations for the contents of performance standards for building components and assemblies and indicates a standard order for their presentation.
NAVY - MIL-D-17984A - DATA PRESENTATION REQUIREMENTS, INSTALLED ENGINE PERFORMANCE AND AIR INDUCTION SYSTEMS Organization: NAVY
Date: 1956-05-01
Description: This specification covers requirements for presentation of performance characteristics of power plant installations and inlet geometry systems, as follows, for all ramjet, pulse jet, turbojet, turboprop, and other air-breathing-type propulsion systems other than reciprocating engines for all piloted aircraft, guided missiles, and target drones: (a) The basic engine performance data, corrected for installation effects, to be presented as the source of the values of power available in calculating aircraft performance under the Navy requirements of Specification MIL-D-8706 and Bureau of Aeronautics publication SAR-304, or Air Force requirements of Specifications MIL-D-8034 and MIL-D-7579.
NPFC - DI-MISC-81966 - GAS TURBINE ENGINE STEADY STATE AND TRANSIENT PERFORMANCE PRESENTATIONS FOR COMPUTER PROGRAMS Organization: NPFC
Date: 2014-07-02
Description: Use/Relationship: Engine steady state and transient computer programs (herein referred to as Models) provide a detailed description of the aerothermodynamic cycle performance and stability characteristics of the Propulsion System.
SAE ARP5571 - (R) GAS TURBINE ENGINE PERFORMANCE PRESENTATION AND NOMENCLATURE FOR OBJECT-ORIENTED COMPUTER PROGRAMS Organization: SAE
Date: 2013-10-01
Description: This document provides recommendations for several aspects of air-breathing gas turbine engine performance modeling using object-oriented programming systems.
SAE ARP4191 - GAS TURBINE ENGINE PERFORMANCE PRESENTATION FOR DIGITAL COMPUTER PROGRAMS USING FORTRAN 77 Organization: SAE
Date: 2009-05-01
Description: This SAE Aerospace Recommended Practice (ARP) provides a method for digital computer programs for gas turbine engine performance, steady-state or transient, performance to be written using the FORTRAN 77 Language.
SAE AS4191 - (R) GAS TURBINE ENGINE PERFORMANCE PRESENTATION FOR COMPUTER PROGRAMS USING FORTRAN Organization: SAE
Date: 2015-10-01
Description: This SAE Aerospace Standard (AS) provides a method for gas turbine engine performance computer programs to be written using Fortran COMMON blocks.
NPFC - DI-MISC-80672 - GAS TURBINE ENGINE STEADY STATE AND TRANSIENT PERFORMANCE PRESENTATIONS FOR DIGITAL COMPUTER PROGRAMS Organization: NPFC
Date: 1988-08-11
NPFC - DI-MSSM-81966 - GAS TURBINE ENGINE STEADY STATE AND TRANSIENT PERFORMANCE PRESENTATIONS FOR COMPUTER PROGRAMS Organization: NPFC
Date: 2015-05-11

1 - 20 of 575 results