Wind Tunnel Investigation Of Aerodynamic Loads On Weapons Separated From Carriage Under The Wing Of A Tactical Fighter Aircraft At Supersonic Speeds
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Author |
: J. C. Donaldson |
Publisher |
: |
Total Pages |
: 212 |
Release |
: 1973 |
ISBN-10 |
: UOM:39015104952760 |
ISBN-13 |
: |
Rating |
: 4/5 (60 Downloads) |
Synopsis Wind Tunnel Investigation of Aerodynamic Loads on Weapons Separated from Carriage Under the Wing of a Tactical Fighter Aircraft at Supersonic Speeds by : J. C. Donaldson
Exploratory static-stability tests were made on models of the MK-84 weapon and a modular weapon configuration during simulated weapon separation from the wing of the F-4C Tactical Fighter Aircraft at freestream Mach numbers 1.76, 2.0, and 2.5. Data were obtained with the parent aircraft at zero angle of attack and the weapon at the carriage incidence angle of -1 deg. Supplementary data were obtained for weapon angles of attack of + or - deg. Unit Reynolds number ranged from 4.6 million per ft at M free stream mach number = 1.76 to 6.2 million per ft at M free stream mach number = 2.5. Selected results are presented which show the effects on the weapon aerodynamic loads of free-stream Mach number, weapon angle of attack, weapon axial position, and the presence of other stores. Representative shadowgraph and schlieren photographs of the interference flow field are also presented. (Author).
Author |
: |
Publisher |
: |
Total Pages |
: 0 |
Release |
: 1973 |
ISBN-10 |
: OCLC:227682790 |
ISBN-13 |
: |
Rating |
: 4/5 (90 Downloads) |
Synopsis Wind Tunnel Investigation of Aerodynamic Loads on Weapons Separated from Carriage Under The Wing of a Tactical Fighter Aircraft at Supersonic Speeds by :
Exploratory static-stability tests were made on models of the MK-84 weapon and a modular weapon configuration during simulated weapon separation from the wing of the F-4C Tactical Fighter Aircraft at freestream Mach numbers 1.76, 2.0, and 2.5. Data were obtained with the parent aircraft at zero angle of attack and the weapon at the carriage incidence angle of -1 deg. Supplementary data were obtained for weapon angles of attack of + or - deg. Unit Reynolds number ranged from 4.6 million per ft at M free stream mach number = 1.76 to 6.2 million per ft at M free stream mach number = 2.5. Selected results are presented which show the effects on the weapon aerodynamic loads of free-stream Mach number, weapon angle of attack, weapon axial position, and the presence of other stores. Representative shadowgraph and schlieren photographs of the interference flow field are also presented. (Author).
Author |
: |
Publisher |
: |
Total Pages |
: 0 |
Release |
: 1973 |
ISBN-10 |
: OCLC:227682790 |
ISBN-13 |
: |
Rating |
: 4/5 (90 Downloads) |
Synopsis Wind Tunnel Investigation of Aerodynamic Loads on Weapons Separated from Carriage Under The Wing of a Tactical Fighter Aircraft at Supersonic Speeds by :
Exploratory static-stability tests were made on models of the MK-84 weapon and a modular weapon configuration during simulated weapon separation from the wing of the F-4C Tactical Fighter Aircraft at freestream Mach numbers 1.76, 2.0, and 2.5. Data were obtained with the parent aircraft at zero angle of attack and the weapon at the carriage incidence angle of -1 deg. Supplementary data were obtained for weapon angles of attack of + or - deg. Unit Reynolds number ranged from 4.6 million per ft at M free stream mach number = 1.76 to 6.2 million per ft at M free stream mach number = 2.5. Selected results are presented which show the effects on the weapon aerodynamic loads of free-stream Mach number, weapon angle of attack, weapon axial position, and the presence of other stores. Representative shadowgraph and schlieren photographs of the interference flow field are also presented. (Author).
Author |
: A. R. Rudnicki (Jr.) |
Publisher |
: |
Total Pages |
: 170 |
Release |
: 1975 |
ISBN-10 |
: UOM:39015104958049 |
ISBN-13 |
: |
Rating |
: 4/5 (49 Downloads) |
Synopsis External Store Airloads Prediction Technique by : A. R. Rudnicki (Jr.)
Author |
: United States. Naval Air Systems Command |
Publisher |
: |
Total Pages |
: 148 |
Release |
: 1975 |
ISBN-10 |
: UIUC:30112104133035 |
ISBN-13 |
: |
Rating |
: 4/5 (35 Downloads) |
Synopsis Technical Information Indexes by : United States. Naval Air Systems Command
Author |
: United States. Congress. House. Committee on Appropriations. Subcommittee on HUD-Independent Agencies |
Publisher |
: |
Total Pages |
: 1112 |
Release |
: 1985 |
ISBN-10 |
: UCAL:B4292990 |
ISBN-13 |
: |
Rating |
: 4/5 (90 Downloads) |
Synopsis National Aeronautics and Space Administration by : United States. Congress. House. Committee on Appropriations. Subcommittee on HUD-Independent Agencies
Author |
: |
Publisher |
: |
Total Pages |
: 156 |
Release |
: 1978 |
ISBN-10 |
: CORNELL:31924057184859 |
ISBN-13 |
: |
Rating |
: 4/5 (59 Downloads) |
Synopsis Technical Abstract Bulletin by :
Author |
: |
Publisher |
: |
Total Pages |
: 648 |
Release |
: 1982 |
ISBN-10 |
: UIUC:30112104409450 |
ISBN-13 |
: |
Rating |
: 4/5 (50 Downloads) |
Synopsis Scientific and Technical Aerospace Reports by :
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Author |
: J. M. Wright |
Publisher |
: |
Total Pages |
: 126 |
Release |
: 1978 |
ISBN-10 |
: UOM:39015104954113 |
ISBN-13 |
: |
Rating |
: 4/5 (13 Downloads) |
Synopsis Documentation of a Transonic Wind Tunnel Test to Investigate the Separation Characteriscis of the GBU-10C/B, the CBU-58, and the BL-755 Stores from the F-16 Aircraft by : J. M. Wright
Author |
: |
Publisher |
: |
Total Pages |
: 52 |
Release |
: 1962 |
ISBN-10 |
: NASA:31769000462583 |
ISBN-13 |
: |
Rating |
: 4/5 (83 Downloads) |
Synopsis Wind Tunnel Investigation of a Supersonic Fan-in-fuselage VTOL Fighter Model at Zero and Low Forward Speeds by :