Supersonic Cruise Research 79: Part 1.

Abstract

Since 1972 the Supersonic Cruise Research (SCR) Program has provided an accelerated and focused technology effort which has resulted in development of improved analytical techniques, design procedures, and an expanded experimental data base. Progress made in the first 4 years was highlighted in a conference at Langley Research Center in 1976 (see NASA CP-0O1, Parts 1 and 2) Subsequent to the 1976 conference, NASA had conducted and monitored additional supersonic cruise vehicle studies and enhanced the advanced supersonic technology data base through further tests. Significant achievements in the interim since the previous conference were reported to the technical community at the SCR 79 Conference held at Langley Research Center, November 13-16, 1979. This document is a compilation of papers, authored by representatives of airframe and engine manufacturers, the Federal Aviation Administration, three NASA research centers, and the Office of Technology Assessment (Congress of the United States) which were presented at the latter Conference. (MM)

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Document Details

Document Type
Technical Report
Publication Date
Nov 16, 1979
Accession Number
ADA305643

Entities

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms
  • Cyber
  • Energy and Power Technologies
  • Ground and Sea Platforms
  • Space

DTIC Thesaurus Topics

  • Aerodynamic Configurations
  • Aircraft Equipment
  • Aircraft Industry
  • Aircrafts
  • Airframes
  • Boundary Layer
  • Commercial Aircraft
  • Computational Fluid Dynamics
  • Flow Visualization
  • Fluid Dynamics
  • High Lift Devices
  • Supersonic Aircraft
  • Swept Wings
  • Test And Evaluation
  • Test Facilities
  • Turbulent Mixing
  • Two Dimensional

Readers

  • Academic Conference Management
  • Aerospace Engineering
  • Technical Research and Report Writing.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow