Accession Number:

ADA012028

Title:

V/STOL Employing ARL Thrust Augmentation Concepts - Research Test Vehicle Configuration Summary and Design Technology Report.

Descriptive Note:

Technical rept. 17 Jul 67-17 Dec 68,

Corporate Author:

BELL AEROSPACE CO BUFFALO N Y

Personal Author(s):

Report Date:

1968-12-01

Pagination or Media Count:

434.0

Abstract:

The results of a detailed preliminary design study of a VSTOL research test vehicle RTV, employing ARL thrust augmentation concepts, are presented. The VSTOL research airplane uses a high by-pass ratio turbofan engine with ejector thrust augmentation in the wing and fuselage nose. Design layouts of all major configuration components and systems are presented together with results of analytical investigations and trade-off studies.

Subject Categories:

  • VSTOL

Distribution Statement:

APPROVED FOR PUBLIC RELEASE