Accession Number:

AD0625820

Title:

HEAVY-LIFT TIP TURBOJET ROTOR SYSTEM. VOLUME 5. STRUCTURAL ANALYSIS

Descriptive Note:

Engineering rept.

Corporate Author:

HILLER AIRCRAFT CORP PALO ALTO CA

Personal Author(s):

Report Date:

1965-10-01

Pagination or Media Count:

129.0

Abstract:

The report discusses stress calculations for major structural components of this system. Tip engine attachment hardware is also analyzed.

Descriptors:

• *HELICOPTER ROTORS
• HELICOPTERS
• LIFT
• STRESSES

Subject Categories:

• Helicopters

Distribution Statement:

APPROVED FOR PUBLIC RELEASE