Flight Measurements Of The Flying Qualities Of Five Light Airplanes
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Flight Measurements of the Flying Qualities of Five Light Airplanes by Paul A. Hunter Pdf
Results are presented of an investigation of stability, controllability, and stalling characteristics of five light airplanes. The effect of slots on the flying qualities of one of the airplanes is also shown. These five airplanes are considerd typical of the light airplanes now being manufactured.
High Speed Problems of Aircraft and Experimental Methods by Allen F. Donovan Pdf
Volume VIII of the High Speed Aerodynamics and Jet Propulsion series. This volume includes: performance calculation at high speed; stability and control of high speed aircraft; aeroelasticity and flutter; model testing; transonic wind tunnels; supersonic tunnels; hypersonic experimental facilities; low density wind tunnels; shock tube; wind tunnel measurements; instrumented models in free flight; piloted aircraft testing; free flight range methods. Originally published in 1961. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.
Flight Measurements of the Flying Qualities of an F6F-3 Airplane (BuAer No. 04776). by Walter C. Williams,John P. Reeder,United States. National Advisory Committee for Aeronautics,Langley Aeronautical Laboratory Pdf
Flight measurements were made of the handling qualities of an F6F-3 airplane. Thirty flights were made covering the period from February 1 to May 15, 1944. This test program was conducted at the Langley Field laboratory of the NACA. The present paper gives results of tests made to determine the longitudinal stability and control of the subject airplane. The remaining portion of the investigation, which includes the lateral and directional stability and control and the stalling characteristics, will be covered in two later reports.
Simulated-altitude Investigations of Performance of Tubular Aircraft Oil Coolers by S. V. Manson Pdf
For constant oil-inlet temperature, congealing of the oil at each altitude produces an initial decrease of about 5 to 10 percent of the maximum heat dissipation attained at the altitude and is followed by constancy of oil hat dissipation as air flow increases.
Investigation of Lateral Control Near the Stall by Fred E. Weick Pdf
Flight tests were made with a typical light airplane to investigate possibilities for obtaining reliable control at low flight speeds. It was found that satisfactory lateral control occurred consistently, even under conditions simulating extremely gusty air, at angles of attack approximately 2 degrees below that for the maximum lift coefficient (or the stall of the wing as a whole). This 2 degree margine was substantially the same both with full power and with the engine throttled and throughout the range of center-of-gravity locations tested. Supplementary tests were then made on the control at high angles of attack under actual gusty air conditions, on the possibility of entering spins, and on the amount of elevator control required for normal three-point landings. It was found that with the original plain untwisted wing obtaining the constant 2 degree margin below the stall required widely different elevator deflections for the range of power and center-of-gravity locations tested. Also, none of these settings ws high enough to produce a three-point landing.
NASA's Contributions to Aeronautics: Flight environment, operations, flight testing, and research by Anonim Pdf
Two-volume collection of case studies on aspects of NACA-NASA research by noted engineers, airmen, historians, museum curators, journalists, and independent scholars. Explores various aspects of how NACA-NASA research took aeronautics from the subsonic to the hypersonic era.-publisher description.
Flight Measurements of the Flying Qualities of an F6F-3 Airplane (BuAer No. 04776). by Walter C. Williams,John P. Reeder,United States. National Advisory Committee for Aeronautics,Langley Aeronautical Laboratory Pdf
Flight measurements were made of the handling qualities of an F6F-3 airplane. The present paper gives results of tests made to determine the lateral and directional stability and control of the subject airplane. The tests covering the stalling characteristics of the F6F-3 airplane will be described in a third report.
Charts Showing Stability and Control Characteristics of Airplanes in Flight by Anonim Pdf
During October 1944, the National Advisory Committee for Aeronautics conducted a series of conferences with the Army, Navy, and representatives of the aircraft industry for the purpose of discussing the flight-test procedures used in measuring the stability and control characteristics of airplanes. The conferences were initiated by the Army Air Forces, Air Technical Service Command, to acquaint the flight organizations of the industry with the flight test methods employed by the NACA and to standardize the techniques insofar as possible as they are employed by the various manufacturers and agencies engaged in determining the flying qualities of airplanes.
