MAXIMUM ALTITUDE AND MAXIMUM MACH NUMBER OBTAINED WITH THE MODIFIED DOUGLAS D-558-II RESEARCH AIRPLANE DURING DEMONSTRATION FLIGHTS

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Document Details

Document Type
Technical Report
Publication Date
Apr 20, 1953
Accession Number
AD0007201

Entities

People

  • Theodore E. Dahlen

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Aircrafts
  • Airplanes
  • Airspeed
  • Altitude
  • Calibration
  • Flight Speeds
  • High Altitude
  • Instrumentation
  • Mach Number
  • Measurement
  • National Security
  • Research Aircraft
  • Sea Level
  • Security
  • Static Pressure
  • Swept Wings