EXPERIMENTAL RESULTS FROM A TEST IN ROUGH AIR AT HIGH SUBSONIC SPEEDS OF A TAILLESS ROCKET MODEL HAVING CRUCIFORM TRIANGULAR WINGS, AND A NOTE ON THE CALCUALTION OF MEAN SQUARE LOADS OF AIRCRAFT IN CONTINUOUS ROUGH AIR

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Document Details

Document Type
Technical Report
Publication Date
Apr 13, 1956
Accession Number
AD0093403

Entities

People

  • A. J. Vitale
  • Jesse L. Mitchell

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Accuracy
  • Aircrafts
  • Airplanes
  • Atmospheric Motion
  • Cruciform Configurations
  • Cruciform Wings
  • Delta Wings
  • Experimental Data
  • Flight
  • Frequency
  • Government Procurement
  • Governments
  • Gust Loads
  • Mach Number
  • Measurement
  • Model Tests
  • Rocket Models