Accession Number:

AD0092432

Title:

INVESTIGATION BY THE TRANSONIC-BUMP METHOD OF A 35 deg SWEPTBACK SEMISPAN MODEL EQUIPPED WITH A FLAP OPERATED BY A SERIES OF SERVOVANES LOCATED AHEAD OF AND GEARED TO THE FLAP

Descriptive Note:

Technical note

Corporate Author:

NATIONAL AERONAUTICS AND SPACE ADMIN LANGLEY RESEARCH CENTER HAMPTON VA

Report Date:

1956-04-01

Pagination or Media Count:

44.0

Abstract:

Subject Categories:

  • Aircraft
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE