Accession Number:

AD0832605

Title:

DESIGN, FABRICATION, TESTING, AND DATA ANALYSIS OF ADAM II CONCEPT (PROPULSIVE WING). PART III, TESTING IN 17 FT TEST SECTION OF 7 FT X 10 FT WIND TUNNEL, NASA LANGLEY RESEARCH CENTER.

Descriptive Note:

Final rept. 2 Dec 66-7 Jul 67,

Corporate Author:

LTV AEROSPACE CORP DALLAS TX VOUGHT AERONAUTICS DIV

Personal Author(s):

• Brownrigg, William E., Jr.
• Meyer, Robert D.
• English, Robert B.

Report Date:

1968-05-01

Pagination or Media Count:

105.0

Abstract:

Descriptors:

• *VERTICAL TAKEOFF AIRCRAFT
• AERODYNAMIC CHARACTERISTICS
• AERODYNAMIC CONTROL SURFACES
• GROUND EFFECT
• INTERFERENCE
• WIND TUNNEL MODELS
• MATHEMATICAL MODELS
• MODEL TESTS
• SCALE
• AERODYNAMIC CONFIGURATIONS
• GAS GENERATING SYSTEMS
• HOVERING
• STABILITY
• THRUST
• SUBSONIC CHARACTERISTICS
• TRANSONIC CHARACTERISTICS
• LEVEL FLIGHT
• TEST FACILITIES
• TEST EQUIPMENT

Subject Categories:

• Aerodynamics
• VSTOL

Distribution Statement:

APPROVED FOR PUBLIC RELEASE