INSTANTANEOUS LOCAL TEMPERATURES OF AERODYNAMIC DECELERATORS. PART I. METHODS OF PREDICTING

Abstract

Identifiers: Parawings.A numerical technique is presented for predicting temperatures developed in aerodynamic decelerators at high speeds. The predictions are obtained both by a simple method to estimate local equilibrium temperatures and by a more complex method to estimate instantaneous, local, temperat re profiles. Sample calculations are included. A new numerical technique is described for predicting one dimensional thermal diffusion. It permits the use of larger time increments and therefore fewer calculations are necessary than with other numerical techniques. (Author)

Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1960
Accession Number
AD0267062

Entities

People

  • G. Engholm
  • R.a. Bambenek
  • R.j. Baschiere

Tags

DTIC Thesaurus Topics

  • Aircraft Wings
  • Airfoils
  • Airframes
  • Diffusion
  • Parawings
  • Thermal Diffusion

Fields of Study

  • Physics

Readers

  • Adaptive Control and Estimation with Uncertainty in Dynamic Systems.
  • Computational Fluid Dynamics (CFD)
  • Fluid Dynamics.