1965-02-01

The Propulsive Wing Turbofan V/STOL 650203

A V/STOL concept has been developed through adherence to a design philosophy of making each decision from the viewpoint of what is best for the overall airplane rather than for one system, such as propulsion. The acronym, ADAM, standing for Air Deflection and Modulation, has been applied to this concept. A typical design for a subsonic recce/strike airplane is described in detail and wind tunnel results are discussed. Performance data are given insofar as security classification permits. The airplane is characterized by a high degree of maneuverability and versatility. Application of the ADAM concept to transport types is treated briefly.

SAE MOBILUS

Subscribers can view annotate, and download all of SAE's content. Learn More »

Access SAE MOBILUS »

Members save up to 16% off list price.
Login to see discount.
Special Offer: Download multiple Technical Papers each year? TechSelect is a cost-effective subscription option to select and download 12-100 full-text Technical Papers per year. Find more information here.
We also recommend:
TECHNICAL PAPER

Aero-Structural Integrated Design of Forward Swept Wing

912021

View Details

TECHNICAL PAPER

Aerodynamics for Formula SAE: A Numerical, Wind Tunnel and On-Track Study

2006-01-0808

View Details

TECHNICAL PAPER

Aerodynamics of Wing Sections for Airplanes

340081

View Details

X