Accession Number:

ADA317838

Title:

Tailless Vectored Fighters Theory. Laboratory and Flight Tests, Including Vectorable Inlets/Nozzles and Tailless Flying Models vs. Pilot's Tolerances Affecting Maximum Post-Stall Vectoring Agility.

Descriptive Note:

Annual rept.

Corporate Author:

TECHNION - ISRAEL INST OF TECH HAIFA FACULTY OF AEROSPACE ENGINEERING

Personal Author(s):

Report Date:

1991-07-01

Pagination or Media Count:

238.0

Abstract:

Presenting the major problems confronting the development, tests and validation of Post-stall PST Thrust-Vectored Fighters TVF, this project is based on the development of an integrated laboratory-flight testing methodology of PST-F-15-TVFRPVs, including the tests of new types of yaw-pitch and roll-yaw-pitch thrust-vectoring nozzles and high-alpha, PST inlets. Mathematical phenomenology of PST-TVF has been added to define the methods required to maximize PST-TV agility and to measure it.

Subject Categories:

  • Attack and Fighter Aircraft
  • Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE