Accession Number : AD0476767


Title :   STRUCTURAL TEMPERATURES AT SUPERSONIC FLIGHT FROM B-58A AND F-105D AIRCRAFT


Descriptive Note : Final rept.


Corporate Author : AIR FORCE FLIGHT DYNAMICS LAB WRIGHT-PATTERSON AFB OH


Personal Author(s) : Durkee, Eugene D


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/476767.pdf


Report Date : Nov 1965


Pagination or Media Count : 73


Abstract : Supersonic flight data are presented from an instrumented B-58A and F-105D aircraft. These data comprise supersonic Mach number, altitude and recorded and predicted temperatures at various wing and fuselage stations. Data presentation is in the form of curves, plots and tables with pertinent descriptive information. These findings are presented to provide a basis for extending the state-of-the-art in structural design criteria for current and future flight vehicles.


Descriptors :   *JET BOMBERS , *JET FIGHTERS , THERMAL PROPERTIES , TEMPERATURE , TIME , MATHEMATICAL PREDICTION , AERODYNAMIC LOADING , WEIGHT , FUSELAGES , AIRFRAMES , INSTRUMENTATION , WINGS , ALTITUDE , SUPERSONIC CHARACTERISTICS , AERODYNAMIC HEATING , THERMOCOUPLES , SKIN FRICTION , CLIMBING


Subject Categories : Aerodynamics
      Fluid Mechanics


Distribution Statement : APPROVED FOR PUBLIC RELEASE