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Thermal Effects on Static Aeroelastic Stability and Control: Part I. Methods of Predictin Structral Temperatures Due to Aerodynamic Heating

Title: Thermal Effects on Static Aeroelastic Stability and Control: Part I. Methods of Predictin Structral Temperatures Due to Aerodynamic Heating
Date: 1959
Index Abstract: Limited
Photo Quality: Incomplete
Report Number: WADC TR 58-378
Creator: Blessing, Arthur H.; Hanawalt, Arnold J.
Corporate Author: Bell Aircraft Corporation
Laboratory: Flight Control Laboratory
Extent: 132
Identifier: AD0237836
Access Rights: ASTIA
Distribution Classification: 2
Contract: AF 33(616)-5014
DoD Project: 1365
DoD Task: 61924
DTIC Record Exists: No
Distribution Change Authority Correspondence: None
Report Availability: Not available via Contrails
Date Issued: 1959-06
Abstract: The abstract for this report is either unavailable or has yet to be entered
Provenance: AFRL/VACA
Type: report