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Longitudinal Stability And Trim Of Two Rocket Propelled Airplane Models Having 45 Sweptback Wings And Tails With The Horizontal Tail Mounted In Two Positions Book in PDF, ePub and Kindle version is available to download in english. Read online anytime anywhere directly from your device. Click on the download button below to get a free pdf file of Longitudinal Stability And Trim Of Two Rocket Propelled Airplane Models Having 45 Sweptback Wings And Tails With The Horizontal Tail Mounted In Two Positions book. This book definitely worth reading, it is an incredibly well-written.
Author : James H. Parks,Alan B. Kehlet
Publisher : Unknown
Page : 36 pages
File Size : 49,8 Mb
Release : 1953
Category : Airplanes
ISBN : UOM:39015086465500
Author : M. Leroy Spearman
Publisher : Unknown
Page : 34 pages
File Size : 50,8 Mb
Release : 1957
Category : Airplanes
ISBN : UOM:39015086466235
An investigation has been conducted in the Langley 4- by 4-foot supersonic pressure tunnel to determine the effects of wing and horizontal-tail vertical location on the aerodynamic characteristics in sideslip at various angles of attack for a supersonic airplane configuration at Mach numbers of 1.41 and 2.01. The basic model was equipped with a wing and horizontal tail, each having 45 degree sweep and an aspect ratio of 4. The wing had a taper ratio of 0.2 and NACA 65A004 sections; the horizontal tail had a taper ratio of 0.4 and NACA 65A006 sections.
Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 580 pages
File Size : 41,6 Mb
Release : 1956
Category : Aeronautics
ISBN : UCBK:C029901318
Author : Anonim
Publisher : Unknown
Page : 818 pages
File Size : 47,8 Mb
Release : 1954
Category : Aeronautics
ISBN : UVA:X004173286
Author : Defense Documentation Center (U.S.)
Publisher : Unknown
Page : 308 pages
File Size : 55,5 Mb
Release : 1960
Category : Science
ISBN : STANFORD:36105016669785
Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 508 pages
File Size : 47,9 Mb
Release : 1954
Category : Aeronautics
ISBN : IND:30000098603164
Author : Anonim
Publisher : Unknown
Page : 34 pages
File Size : 55,9 Mb
Release : 1983
Category : Electronic
ISBN : NASA:31769000558919
Author : Joseph Adams Shortal
Publisher : Unknown
Page : 808 pages
File Size : 50,6 Mb
Release : 1978
Category : Aeronautics
ISBN : STANFORD:36105024718376
Author : National Research Council Canada
Publisher : Unknown
Page : 762 pages
File Size : 43,5 Mb
Release : 1960
Category : Aeronautics
ISBN : UOM:39015023950788
Author : National Aeronautical Establishment (Canada)
Publisher : Unknown
Page : 478 pages
File Size : 40,6 Mb
Release : 195?
Category : Aeronautics
ISBN : PURD:32754086683236
Author : Zbigniew Krzywoblocki (|d)
Publisher : Unknown
Page : 170 pages
File Size : 47,6 Mb
Release : 1957
Category : Aerodynamics
ISBN : UOM:39015095330323
Author : Anonim
Publisher : Unknown
Page : 1364 pages
File Size : 42,6 Mb
Release : 1951
Category : Government publications
ISBN : WISC:89117116129
Author : United States. Superintendent of Documents
Publisher : Unknown
Page : 1366 pages
File Size : 42,8 Mb
Release : 1968
Category : United States
ISBN : STANFORD:36105022657535
Author : Reginald R. Lundstrom
Publisher : Unknown
Page : 48 pages
File Size : 53,8 Mb
Release : 1957
Category : Aerodynamics, Supersonic
ISBN : UOM:39015086490490
Two rocket models having cruciform, aspect-ratio-5, unwswept tails and a fineness-ratio-20 fuselage were flight tested over a Mach number range of approximately 1.7 to 2.4. One of the models had cruciform, aspect-ratio-3.4 forward surfaces in line with the tails. The models were given step disturbances by pulse rockets at intervals throughout the Mach number range and stability derivatives were obtained from the measured responses. The roll rates of the models varied from 10 radians per second to 5 radians per second.
Author : Robert F. Peck,Jesse L. Mitchell
Publisher : Unknown
Page : 32 pages
File Size : 46,5 Mb
Release : 1953
Category : Delta wing airplanes
ISBN : UOM:39015095100668