Accession Number:

AD0249771

Title:

STRUCTURAL TEST PROGRAM F-106A AIRPLANE

Descriptive Note:

Corporate Author:

WRIGHT AIR DEVELOPMENT DIV WRIGHT-PATTERSON AFB OH ENGINEERING TEST DIV

Personal Author(s):

• Lustig, Sanford
• Jackson, David W.
• Hussong, Fred E.

Report Date:

1960-08-01

Pagination or Media Count:

72.0

Abstract:

The F-106 airplane was subjected to a complete static test program covering all of the critical flight, landing and ground handling conditions.

Descriptors:

• *SIMULATION
• *LOAD DISTRIBUTION
• *JET FIGHTERS
• FLIGHT TESTING
• AIRFRAMES
• INSTRUMENTATION
• AERODYNAMIC HEATING
• ALL WEATHER AVIATION
• LANDING GEAR

Subject Categories:

• Attack and Fighter Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE