NASA Technical Note

NASA Technical Note
Author :
Publisher :
Total Pages : 424
Release :
ISBN-10 : MINN:319510008462661
ISBN-13 :
Rating : 4/5 (61 Downloads)

Synopsis NASA Technical Note by :

Aerodynamics of V/STOL Flight

Aerodynamics of V/STOL Flight
Author :
Publisher : Courier Corporation
Total Pages : 356
Release :
ISBN-10 : 0486404609
ISBN-13 : 9780486404608
Rating : 4/5 (09 Downloads)

Synopsis Aerodynamics of V/STOL Flight by : Barnes Warnock McCormick

An extremely practical overview of V/STOL (vertical/short takeoff and landing) aerodynamics, this volume offers a presentation of general theoretical and applied aerodynamic principles, covering propeller and helicopter rotor theory for both the static and forward flight cases. Both a text for students and a reference for professionals, the book can be used for advanced undergraduate or graduate courses. Numerous detailed figures, plus exercises. 1967 edition. Preface. Appendix. Index.

An Examination of Handling Qualities Criteria for V/STOL Aircraft

An Examination of Handling Qualities Criteria for V/STOL Aircraft
Author :
Publisher :
Total Pages : 56
Release :
ISBN-10 : UIUC:30112106588822
ISBN-13 :
Rating : 4/5 (22 Downloads)

Synopsis An Examination of Handling Qualities Criteria for V/STOL Aircraft by : Seth B. Anderson

A study has been undertaken to define hand-ling qualities criteria for V/STOL aircraft. With the current military requirements for helicopters and airplanes as a framework, modifications and additions were made for conversion to a preliminary set of V/STOL requirements using a broad background of flight experience and pilots' comments from VTOL and STOL aircraft, BLC (boundary-layer-control) equipped aircraft, variable stability aircraft, flight simulators and landing approach studies. The report contains a discussion of the reasoning behind and the sources of information leading to suggested requirements. The results of the study indicate that the majority of V/STOL requirements can be defined by modifications to the helicopter and/or airplane requirements by appropriate definition of reference speeds. Areas where a requirement is included but where the information is felt to be inadequate to establish a firm quantitative requirement include the following: Control power and damping relationships about all axes for various sizes and types of aircraft; control power, sensitivity, d-amping and response for height control; dynamic longitudinal and dynamic lateral- directional stability in the transition region, including emergency operation; hovering steadiness; acceleration and deceleration in transition; descent rates and flight-path angles in steep approaches, and thrust margin for approach.

NASA's Contributions to Aeronautics: Flight environment, operations, flight testing, and research

NASA's Contributions to Aeronautics: Flight environment, operations, flight testing, and research
Author :
Publisher :
Total Pages : 1064
Release :
ISBN-10 : UCSD:31822036341212
ISBN-13 :
Rating : 4/5 (12 Downloads)

Synopsis NASA's Contributions to Aeronautics: Flight environment, operations, flight testing, and research by :

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.

U.S. Aeronautics and Space Activities

U.S. Aeronautics and Space Activities
Author :
Publisher :
Total Pages : 540
Release :
ISBN-10 : UCR:31210025389162
ISBN-13 :
Rating : 4/5 (62 Downloads)

Synopsis U.S. Aeronautics and Space Activities by : United States. President