Accession Number:

ADA318761

Title:

Dynamic Scaling of Prototypes Using Radius of Gyration Method: Theory, Laboratory and Flight Tests.

Descriptive Note:

Final rept. 1 Aug-20 Dec 91,

Corporate Author:

TECHNION - ISRAEL INST OF TECH HAIFA JET PROPULSION LAB

Personal Author(s):

Report Date:

1991-12-01

Pagination or Media Count:

157.0

Abstract:

The potential introduction of new Post-Stall PST, air-to-air and air-to-ground maneuvers and tactics via thrust-vectoring control TVC may dramatically increase fighter-aircraft performance at low subsonic speeds. TVC is now expected to double or triple maximum nose turning rates, especially under nonconventional, rapid, rigid-body-type-rotationstranslations, or during PST-updown whippings. It is also expected to expand flight envelopes beyond conventional limits, reduce signatures, improve STOL capabilities and enhance safety margins, especially at takeoff and landing and in the prevention or recovery from any spin situation. This interim Progress Report deals with the generation of such data for future USAF PST-TVF-16S.

Subject Categories:

  • Aerodynamics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE