National Technical Reports Library - NTRL

National Technical Reports Library

The National Technical Information Service acquires, indexes, abstracts, and archives the largest collection of U.S. government-sponsored technical reports in existence. The NTRL offers online, free and open access to these authenticated government technical reports. Technical reports and documents in its repository may be available online for free either from the issuing federal agency, the U.S. Government Publishing Office’s Federal Digital System website, or through search engines.




Details
Actions:

F-105F Transonic Buffet Study and Effect of Maneuvering Flaps.


AD693650

Publication Date 1969
Personal Author Margolin, M.; Chung, J. G.
Page Count 224
Abstract The objective of the test program reported herein was the evaluation of maneuvering flaps as a means of increasing the lift of a high performance aircraft at the onset of Mach buffet and decreasing the level of buffet intensity so that the total maneuvering range of the aircraft is increased. The results of this evaluation are presented in this report. (Author)
Keywords
  • Jet fighters
  • Transonic characteristics
  • Buffeting
  • Leading edge flaps
  • Trailing control surfaces
  • Boundary layer transition
  • Drag
  • Angle of attack
  • Lift
  • Vibration
  • Resonant frequency
  • Wind tunnel models
  • Flight testing
  • Statistical analysis
  • F-105 aircraft
  • F-105F aircraft
  • Trailing edge flaps
NTIS Subject Category
  • 51C - Aircraft
  • 46B - Fluid Mechanics
Corporate Authors Fairchild Hiller Corp Farmingdale N Y Republic Aviation Div
Document Type Technical Report
Title Note Final technical rept. 29 Mar 68-1 Apr 69.
NTIS Issue Number 196921
Contract Number
  • F33657-68-C-1057
F-105F Transonic Buffet Study and Effect of Maneuvering Flaps.
F-105F Transonic Buffet Study and Effect of Maneuvering Flaps.
AD693650

  • Jet fighters
  • Transonic characteristics
  • Buffeting
  • Leading edge flaps
  • Trailing control surfaces
  • Boundary layer transition
  • Drag
  • Angle of attack
  • Lift
  • Vibration
  • Resonant frequency
  • Wind tunnel models
  • Flight testing
  • Statistical analysis
  • F-105 aircraft
  • F-105F aircraft
  • Trailing edge flaps
  • 51C - Aircraft
  • 46B - Fluid Mechanics
  • F33657-68-C-1057
Loading